Knowledge (XXG)

Buckling

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bend significantly and the material of the column will diverge from a linear stress-strain behavior. The stress-strain behavior of materials is not strictly linear even below the yield point, hence the modulus of elasticity decreases as stress increases, and significantly so as the stresses approach the material's yield strength. This reduced material rigidity reduces the buckling strength of the structure and results in a buckling load less than that predicted by the assumption of linear elastic behavior.
3111:, which is less than the elastic modulus, in place of the elastic modulus of elasticity. The tangent is equal to the elastic modulus and then decreases beyond the proportional limit. The tangent modulus is a line drawn tangent to the stress-strain curve at a particular value of strain (in the elastic section of the stress-strain curve, the tangent modulus is equal to the elastic modulus). Plots of the tangent modulus of elasticity for a variety of materials are available in standard references. 2781:. If the beam is not supported in the lateral direction (i.e., perpendicular to the plane of bending), and the flexural load increases to a critical limit, the beam will experience a lateral deflection of the compression flange as it buckles locally. The lateral deflection of the compression flange is restrained by the beam web and tension flange, but for an open section the twisting mode is more flexible, hence the beam both twists and deflects laterally in a failure mode known as 357:. At that load, the introduction of the slightest lateral force will cause the column to fail by suddenly "jumping" to a new configuration, and the column is said to have buckled. This is what happens when a person stands on an empty aluminum can and then taps the sides briefly, causing it to then become instantly crushed (the vertical sides of the can may be understood as an infinite series of extremely thin columns). The formula derived by Euler for long slender columns is 4175: 2762: 253: 3168:
wave to travel along the column to the other (free) end and back down as a relief wave. Maximum buckling occurs near the impact end at a wavelength much shorter than the length of the rod, and at a stress many times the buckling stress of a statically loaded column. The critical condition for buckling amplitude to remain less than about 25 times the effective rod straightness imperfection at the buckle wavelength is
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that member, the member will continue to support the load that caused it to buckle. If the buckled member is part of a larger assemblage of components such as a building, any load applied to the buckled part of the structure beyond that which caused the member to buckle will be redistributed within the structure. Some aircraft are designed for thin skin panels to continue carrying load even in the buckled state.
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boundary conditions, when a plate is loaded with a critical stress and buckles, the edges perpendicular to the load cannot deform out-of-plane and will therefore continue to carry the stresses. This creates a non-uniform compressive loading along the ends, where the stresses are imposed on half of the effective width on either side of the specimen, given by the following:
4063: 4015: 747: 34: 4123: 3614: 1406: 283:. A load at any other point in the cross section is known as an eccentric load. A short column under the action of an axial load will fail by direct compression before it buckles, but a long column loaded in the same manner will fail by springing suddenly outward laterally (buckling) in a bending mode. The buckling mode of 4422:
Aerothermal heating can lead to buckling of surface panels on super- and hypersonic aerospace vehicles such as high-speed aircraft, rockets and reentry vehicles. If buckling is caused by aerothermal loads, the situation can be further complicated by enhanced heat transfer in areas where the structure
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columns may be classified as short columns if the ratio of the length to least dimension of the cross section is equal to or less than 10. The dividing line between intermediate and long timber columns cannot be readily evaluated. One way of defining the lower limit of long timber columns would be to
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consists of a thin rim kept under high compressive stress by the (roughly normal) inward pull of a large number of spokes. It can be considered as a loaded column that has been bent into a circle. If spoke tension is increased beyond a safe level or if part of the rim is subject to a certain lateral
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is a 3-dimensional structure defined as having a width of comparable size to its length, with a thickness that is very small in comparison to its other two dimensions. Similar to columns, thin plates experience out-of-plane buckling deformations when subjected to critical loads; however, contrasted
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Another insight that may be gleaned from this equation is the effect of length on critical load. Doubling the unsupported length of the column quarters the allowable load. The restraint offered by the end connections of a column also affects its critical load. If the connections are perfectly rigid
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The boundary conditions have a considerable effect on the critical load of slender columns. The boundary conditions determine the mode of bending of the column and the distance between inflection points on the displacement curve of the deflected column. The inflection points in the deflection shape
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The buckling strength of a member is less than the elastic buckling strength of a structure if the material of the member is stressed beyond the elastic material range and into the non-linear (plastic) material behavior range. When the compression load is near the buckling load, the structure will
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column is one whose slenderness ratio does not exceed 50; an intermediate length steel column has a slenderness ratio ranging from about 50 to 200, and its behavior is dominated by the strength limit of the material, while a long steel column may be assumed to have a slenderness ratio greater than
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If a column is loaded suddenly and then the load released, the column can sustain a much higher load than its static (slowly applied) buckling load. This can happen in a long, unsupported column used as a drop hammer. The duration of compression at the impact end is the time required for a stress
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allows for an increase of the number of sine waves produced by buckling along the length, but also increases the resistance from the buckling along the width. This creates the preference of the plate to buckle in such a way to equal the number of curvatures both along the width and length. Due to
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in the material of which the structure is composed. Further loading may cause significant and somewhat unpredictable deformations, possibly leading to complete loss of the member's load-carrying capacity. However, if the deformations that occur after buckling do not cause the complete collapse of
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displacement, the fundamental path is shown. It demonstrates the plate's similarity to a column under buckling; however, past the buckling load, the fundamental path bifurcates into a secondary path that curves upward, providing the ability to be subjected to higher loads past the critical load.
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Since structural columns are commonly of intermediate length, the Euler formula has little practical application for ordinary design. Issues that cause deviation from the pure Euler column behaviour include imperfections in geometry of the column in combination with plasticity/non-linear stress
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A conclusion from the above is that the buckling load of a column may be increased by changing its material to one with a higher modulus of elasticity (E), or changing the design of the column's cross section so as to increase its moment of inertia. The latter can be done without increasing the
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is considered a failure mode, and it generally occurs before the axial compression stresses (direct compression) can cause failure of the material by yielding or fracture of that compression member. However, intermediate-length columns will fail by a combination of direct compressive stress and
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Often it is very difficult to determine the exact buckling load in complex structures using the Euler formula, due to the difficulty in determining the constant K. Therefore, maximum buckling load is often approximated using energy conservation and referred to as an energy method in structural
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The Federal Railroad Administration issued a Safety Advisory on July 11, 2012 alerting railroad operators to inspect tracks for "buckling-prone conditions." The Advisory included a brief summary of four derailments that had occurred between June 23 to July 4 that appeared to be "heat related
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Flexural-torsional buckling can be described as a combination of bending and twisting response of a member in compression. Such a deflection mode must be considered for design purposes. This mostly occurs in columns with "open" cross-sections and hence have a low torsional stiffness, such as
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As the loaded stress increases, the effective width continues to shrink; if the stresses on the ends ever reach the yield stress, the plate will fail. This is what allows the buckled structure to continue supporting loadings. When the axial load over the critical load is plotted against the
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The first step in this method is to assume a displacement mode and a function that represents that displacement. This function must satisfy the most important boundary conditions, such as displacement and rotation. The more accurate the displacement function, the more accurate the result.
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of the column are the points at which the curvature of the column changes sign and are also the points at which the column's internal bending moments of the column are zero. The closer the inflection points are, the greater the resulting axial load capacity (bucking load) of the column.
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Sun kink can lead to railroads drastically reducing the speed of trains, leading to delays and cancellations. This is done to avoid derailment. Intensifying heat waves due to climate change doubled the number of hours of heat related delays in 2023, compared to 2018.
2785:. In wide-flange sections (with high lateral bending stiffness), the deflection mode will be mostly twisting in torsion. In narrow-flange sections, the bending stiffness is lower and the column's deflection will be closer to that of lateral bucking deflection mode. 41:
aircraft. Thin skin panels buckle at very low loads. In the case shown here, the weight of the forward fuselage structure ahead of the nose undercarriage is sufficient to cause the panels to buckle. Buckled panels are still effective in carrying shear by diagonal
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strain behaviour of the column's material. Consequently, a number of empirical column formulae have been developed that agree with test data, all of which embody the slenderness ratio. Due to the uncertainty in the behavior of columns, for design, appropriate
1647:{\displaystyle {\frac {\partial ^{4}w}{\partial x^{4}}}+2{\frac {\partial ^{4}w}{\partial x^{2}\partial y^{2}}}+{\frac {\partial ^{4}w}{\partial y^{4}}}={\frac {12\left(1-\nu ^{2}\right)}{Et^{3}}}\left(-N_{x}{\frac {\partial ^{2}w}{\partial x^{2}}}\right)} 2515: 272:(sometimes expressed with the Greek letter lambda, λ). This ratio affords a means of classifying columns and their failure mode. The slenderness ratio is important for design considerations. All the following are approximate values used for convenience. 3420:
In this method, there are two equations used (for small deformations) to approximate the "strain" energy (the potential energy stored as elastic deformation of the structure) and "applied" energy (the work done on the system by external forces).
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The method assumes that the system (the column) is a conservative system in which energy is not dissipated as heat, hence the energy added to the column by the applied external forces is stored in the column in the form of strain energy.
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to column buckling, plates under buckling loads can continue to carry loads, called local buckling. This phenomenon is incredibly useful in numerous systems, as it allows systems to be engineered to provide greater loading capacities.
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Since the radius of gyration is defined as the square root of the ratio of the column's moment of inertia about an axis to its cross sectional area, the above Euler formula may be reformatted by substituting the radius of gyration
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Diagonal tension may also result in a pulling force on any fasteners such as rivets that are used to fasten the web to the supporting members. Fasteners and sheets must be designed to resist being pulled off their supports.
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weight of the column by distributing the material as far from the principal axis of the column's cross section as possible. For most purposes, the most effective use of the material of a column is that of a tubular section.
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Because of the thin skins typically used in aerospace applications, skins may buckle at low load levels. However, once buckled, instead of being able to transmit shear forces, they are still able to carry load through
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column is one having a ratio of unsupported length to least dimension of the cross section equal to or less than 10. If the ratio is greater than 10, it is considered a long column (sometimes referred to as a slender
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A demonstration model illustrating the different "Euler" buckling modes. The model shows how the boundary conditions affect the critical load of a slender column. The columns are identical, apart from the boundary
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Sheets under diagonal tension are supported by stiffeners that as a result of sheet buckling carry a distributed load along their length, and may in turn result in these structural members failing under buckling.
4247:") like a three-dimensional Euler column. If this is a purely elastic deformation the rim will resume its proper plane shape if spoke tension is reduced or a lateral force from the opposite direction is applied. 895: 4409:
Pipes and pressure vessels subject to external overpressure, caused for example by steam cooling within the pipe and condensing into water with subsequent massive pressure drop, risk buckling due to compressive
3609:{\displaystyle {\begin{aligned}U_{\text{strain}}&={\frac {E}{2}}\int I(x)(w_{xx}(x))^{2}\,\mathrm {d} x\\U_{\text{applied}}&={\frac {P_{\text{crit}}}{2}}\int (w_{x}(x))^{2}\,\mathrm {d} x\end{aligned}}} 2399: 2353:, and the number of lengthwise curvatures. For an increasing number of such curvatures, the aspect ratio produces a varying buckling coefficient; but each relation provides a minimum value for each 3132:(DT) stresses in the web. This results in a non-linear behaviour in the load carrying behaviour of these details. The ratio of the actual load to the load at which buckling occurs is known as the 3416: 430: 3431: 3140:
of the wrinkles. Although they may buckle, thin sheets are designed to not permanently deform and return to an unbuckled state when the applied loading is removed. Repeated buckling may lead to
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when determining lateral-torsional buckling. The reason for this factor is to allow for non-uniform moment diagrams when the ends of a beam segment are braced. The conservative value for
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Sections that are made up of flanged plates such as a channel, can still carry load in the corners after the flanges have locally buckled. Crippling is failure of the complete section.
78:. If a structure is subjected to a gradually increasing load, when the load reaches a critical level, a member may suddenly change shape and the structure and component is said to have 2765:
Lateral-torsional buckling of an I-beam with vertical force in center: a) longitudinal view, b) cross section near support, c) cross section in center with lateral-torsional buckling
4275:, forcing adjacent pieces to push against each other. If the stress is sufficient, the pavement can lift and crack without warning. Traversing a buckled section can be jarring to 3210: 2708: 2075: 653: 4113: 3755: 209: 2737: 931: 4219: 4167: 3002: 1139: 973:
which estimates the critical buckling load based on an assumed small initial curvature, hence an eccentricity of the axial load. The Rankine Gordon formula, named for
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set it as the smallest value of the ratio of length to least cross sectional area that would just exceed a certain constant K of the material. Since K depends on the
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For a rectangular plate, supported along every edge, loaded with a uniform compressive force per unit length, the derived governing equation can be stated by:
760:(not allowing rotation of its ends), the critical load will be four times that for a similar column where the ends are pinned (allowing rotation of its ends). 2229: 4893:
Spottswood, S. Michael; Beberniss, Timothy J.; Eason, Thomas G.; Perez, Ricardo A.; Donbar, Jeffrey M.; Ehrhardt, David A.; Riley, Zachary B. (March 2019).
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Elishakoff, I. Li Y-W. and Starnes, J.H. Jr., Non Classical Problems in the Theory of Elastic Stability, Cambridge University Press, 2001, XVI +pp.336;
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Single-degree-of-freedom (SDoF) rigid link models depicting four distinct types of buckling phenomena. The spring in each model is unstressed when
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channels, structural tees, double-angle shapes, and equal-leg single angles. Circular cross sections do not experience such a mode of buckling.
3930:. Simple models for each of these types of buckling behaviour are shown in the figures below, along with the associated bifurcation diagrams. 3722:, it is possible to identify four fundamental forms of buckling found in structural models with one degree of freedom. We start by expressing 202: 4846: 5097: 5069: 4562: 4708: 4414:. Design rules for calculation of the required wall thickness or reinforcement rings are given in various piping and pressure vessel codes. 1921:{\displaystyle w=\sum _{m=1}^{\infty }\sum _{n=1}^{\infty }w_{mn}\sin \left({\frac {m\pi x}{a}}\right)\sin \left({\frac {n\pi y}{b}}\right)} 3151:
Thicker plates may only partially form a diagonal tension field and may continue to carry some of the load through shear. This is known as
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From the derived equations, it can be seen the close similarities between the critical stress for a column and for a plate. As the width
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and Perry Hugesworth Gordon (1899 – 1966), is also based on experimental results and suggests that a column will buckle at a load
5139: 4665: 4518: 195: 339:, that gives the maximum axial load that a long, slender, ideal column can carry without buckling. An ideal column is one that is: 5029:
Rajesh, Dhakal; Maekawa, Koichi (2002). "Reinforcement Stability and Fracture of Cover Concrete in Reinforced Concrete Members".
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When the applied load reaches the Euler load, sometimes called the critical load, the column comes to be in a state of unstable
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shrinks, the plate acts more like a column as it increases the resistance to buckling along the plate's width. The increase of
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is stationary with respect to the coordinate measuring the degree(s) of freedom and that these points are only stable if
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Bifurcation diagrams (blue) for the above models with the energy function (red) animated at different values of load,
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can be taken as 1, regardless of beam configuration or loading, but in some cases it may be excessively conservative.
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Examination of this formula reveals the following facts with regard to the load-bearing ability of slender columns.
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The complete theory and example experimental results for long columns are available as a 39-page PDF document at
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A more accurate approximation of the buckling load can be had by the use of the tangent modulus of elasticity, E
2510:{\displaystyle \sigma _{cr}=k_{cr}{\frac {\pi ^{2}E}{12\left(1-\nu ^{2}\right)\left({\frac {b}{t}}\right)^{2}}}} 4389: 284: 4432: 3841:
in its direction. Using the axioms of elastic instability theory, namely that equilibrium is any point where
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Given stress is found by the load per unit area, the following expression is found for the critical stress:
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of a sheet. High buckling ratios may lead to excessive wrinkling of the sheets which may then fail through
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force, the wheel spontaneously fails into a characteristic saddle shape (sometimes called a "taco" or a "
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Derailment of Amtrak Auto Train P052-18 on the CSXT Railroad Near Crescent City, Florida April 18, 2002
1308:{\displaystyle h_{\text{crit}}=\left({\frac {9B^{2}}{4}}\,{\frac {EI}{\rho gA}}\right)^{\frac {1}{3}}} 4955: 4906: 4371: 3294:
is the smaller lateral dimension of a rectangular rod. Because the buckle wavelength depends only on
720: 227: 59: 5016: 2686: 632: 4838: 4256: 3137: 2778: 183: 153: 118: 4068: 5149: 4986: 4944:"Experiments on High-Temperature Hypersonic Fluid–Structure Interaction with Plastic Deformation" 4924: 4895:"Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions" 4472: 3141: 2793: 2715: 902: 265: 223: 143: 123: 75: 4180: 4128: 3155:(IDT). This behavior was studied by Wagner and these beams are sometimes known as Wagner beams. 2373:. This minimum value can then be used as a constant, independent from both the aspect ratio and 1731: 4530:
Kato, K. (1915). "Mathematical Investigation on the Mechanical Problems of Transmission Line".
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is the maximum compressive load. This formula typically produces a conservative estimate of
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A column under a concentric axial load exhibiting the characteristic deformation of buckling
4047:(black). Note, the load is on the vertical axis. All graphs are in non-dimensional form. 3067: 3038: 3009: 2046: 1684: 1158: 1090: 1063: 661: 574: 440: 256:
The eccentricity of the axial force results in a bending moment acting on the beam element.
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can be separated providing the equation for the critical compressive loading of a plate:
936: 4959: 4910: 4291: 4174: 3670: 691: 4991: 4579: 4449: 4308: 4030: 3864: 3844: 3824: 3780: 3760: 3705: 3650: 3337: 3317: 3277: 3257: 3237: 2542: 2522: 2376: 2356: 2314: 2187:{\displaystyle N_{x,cr}=k_{cr}{\frac {\pi ^{2}Et^{3}}{12\left(1-\nu ^{2}\right)b^{2}}}} 2026: 2002: 1980: 1958: 1936: 1763: 1738: 1662: 1364: 1340: 1320: 1198: 1178: 797: 547: 525: 499: 473: 332: 4457: – method of increasing rigidity and structural integrity of materials or objects 4053: 3881:
is a local minimum and unstable if otherwise (e.g. maximum or a point of inflection).
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The previous equation can be substituted into the earlier differential equation where
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parallel to the grain, it can be seen that this arbitrary limit would vary with the
4316: 4264: 4014: 3984: 1215:, will buckle under its own weight if its height exceeds a certain critical value: 3091:, absolute value of maximum moment at three-quarter point of the unbraced segment, 1784:
The solution to the deflection can be expanded into two harmonic functions shown:
568:, whose value depends on the conditions of end support of the column, as follows. 4463: 4441: – The absorption and transmission of neutrons by nuclear reactor materials 4411: 4304: 4296: 4004: 3974: 2965:{\displaystyle C_{b}={\frac {12.5M_{\max }}{2.5M_{\max }+3M_{A}+4M_{B}+3M_{C}}}} 2792:
will mitigate the effects of lateral-torsional buckling by virtue of their high
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The theory of the behavior of columns was investigated in 1757 by mathematician
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200 and its behavior is dominated by the modulus of elasticity of the material.
4919: 4894: 4595: 4454: 4342: 4315:. It is more common for rails to move laterally, often pulling the underlying 4280: 4276: 2830: 3033:, absolute value of maximum moment at quarter point of the unbraced segment, 1051:{\displaystyle {\frac {1}{F_{\max }}}={\frac {1}{F_{e}}}+{\frac {1}{F_{c}}}} 244: 108: 5114: 4062: 746: 33: 4393: 4244: 3062:, absolute value of maximum moment at centerline of the unbraced segment, 304: 133: 4766:(Report). National Transportation Safety Board. 5 August 2003. p. v 4122: 2770: 2302:{\displaystyle k_{cr}=\left({\frac {mb}{a}}+{\frac {a}{mb}}\right)^{2}} 324: 128: 5051: 4968: 4943: 4839:"Misaligned Track from Heat 'Probable Cause' In Green Line Derailment" 4707:
Li, Dingquing; Hyslip, James; Sussmann, Ted; Chrismer, Steven (2002).
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is not given in tables, it can be obtained via the following formula:
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The buckling coefficient is influenced by the aspect of the specimen,
4358: 4338: 890:{\displaystyle \sigma ={\frac {F}{A}}={\frac {\pi ^{2}E}{(l/r)^{2}}}} 261: 67: 27: 327:
of the timber. The value of K is given in most structural handbooks.
3334:, this same formula holds for thin cylindrical shells of thickness 226:
that develop in the structure are well below those needed to cause
4290: 4173: 4121: 4061: 4052: 4013: 4003: 3983: 3973: 2760: 745: 465: 296: 251: 243: 32: 4557:] (in German). Wein, Austria: J. Springer. pp. 107–109. 1385:
of the first kind of order −1/3, which is equal to 1.86635086...
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bifurcation. All but the first of these examples is a form of
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refer to the first and second derivatives of the displacement.
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Resolution of Twentieth Century Conundrum in Elastic Stability
4435: – Formula to quantify column buckling under a given load 4367: 4347: 4268: 3978:
A tied truss model with inclined links and horizontal spring.
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are introduced into these formulae. One such formula is the
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For one end fixed and the other end free to move laterally,
4736:"Amtrak Passengers Face Record Delays From Extreme Weather" 3004:, absolute value of maximum moment in the unbraced segment, 520:(second moment of area) of the cross section of the column, 16:
Sudden change in shape of a structural component under load
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Nenezich, M. (2004). "Thermoplastic Continuum Mechanics".
4475: – Pattern of buckling used in mechanical engineering 2807:
is a modification factor used in the equation for nominal
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Daub, Dennis; Esser, Burkard; Gülhan, Ali (April 2020).
4683:"Derailments May Increase as 'Sun Kinks' Buckle Tracks" 279:(centroid) of its cross section, it is called an axial 90:
are used to determine the buckling stress of a column.
5092:. Singapore: World Scientific/Imperial College Press. 2829:
is always equal to or greater than 1, never less. For
1953:, number of half sine curvatures that occur lengthwise 933:
is the stress that causes buckling in the column, and
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of the material of the column and not the compressive
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Journal of the Japan Society of Mechanical Engineers
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Pages displaying wikidata descriptions as a fallback
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Pages displaying wikidata descriptions as a fallback
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These accidents were deemed to be sun kink-related (
3411:{\displaystyle U_{\text{applied}}=U_{\text{strain}}} 727:
of the column determines the column's buckling load.
425:{\displaystyle F_{c}={\frac {\pi ^{2}EI}{(KL)^{2}}}} 4812:"Heat could warp train tracks, causing derailments" 4787:"Passenger Train Cars Plunge Off Overheated Tracks" 4990: 4213: 4161: 4107: 4039: 3952: 3873: 3853: 3833: 3813: 3789: 3769: 3749: 3714: 3682: 3659: 3639: 3608: 3410: 3346: 3326: 3306: 3286: 3266: 3246: 3226: 3204: 3083: 3054: 3025: 2996: 2964: 2731: 2702: 2670: 2551: 2531: 2509: 2385: 2365: 2345: 2323: 2301: 2218: 2186: 2062: 2035: 2011: 1989: 1967: 1945: 1920: 1772: 1747: 1722: 1700: 1671: 1646: 1373: 1349: 1329: 1307: 1207: 1187: 1167: 1133: 1106: 1079: 1050: 953: 925: 889: 806: 786: 703: 676: 647: 618: 589: 556: 534: 508: 482: 456: 424: 5081:Analysis and Design of Flight Vehicle Structures 4501:Analysis and Design of Flight Vehicle Structures 4311:, and can fail by buckling, a phenomenon called 3647:is the displacement function and the subscripts 2989: 2906: 2891: 1126: 1001: 4874:(Report). Federal Register. p. 41881-41882 4271:is absorbed in the road surface, causing it to 1155:A free-standing, vertical column, with density 571:For both ends pinned (hinged, free to rotate), 275:If the load on a column is applied through the 3777:is the strain energy stored in the structure, 2833:or overhangs where the free end is unbraced, C 4555:The buckling resistance of members and frames 4551:Die Knickfestigkeit von Stäben und Stabwerken 3884:These four forms of elastic buckling are the 3095:The result is the same for all unit systems. 203: 8: 629:For one end fixed and the other end pinned, 5064:(Fourth ed.). United States: Thomson. 4582:(1998). "The Shape of the Tallest Column". 4259:materials, primarily with concrete, since 2788:The use of closed sections such as square 2769:When a simply supported beam is loaded in 210: 196: 92: 5050: 5043:10.1061/(ASCE)0733-9445(2002)128:10(1253) 4967: 4918: 4637:Lindberg, H. E.; Florence, A. L. (1987). 4494: 4492: 4490: 4488: 4203: 4188: 4182: 4151: 4136: 4130: 4088: 4076: 4070: 4032: 3939: 3866: 3846: 3826: 3806: 3782: 3762: 3727: 3707: 3672: 3652: 3623: 3594: 3593: 3587: 3568: 3547: 3541: 3528: 3512: 3511: 3505: 3483: 3451: 3438: 3430: 3428: 3402: 3389: 3383: 3339: 3319: 3299: 3279: 3259: 3239: 3219: 3193: 3175: 3075: 3069: 3046: 3040: 3017: 3011: 2988: 2982: 2953: 2937: 2921: 2905: 2890: 2880: 2871: 2865: 2723: 2717: 2694: 2688: 2652: 2639: 2632: 2610: 2597: 2591: 2589: 2575: 2569: 2567: 2544: 2524: 2498: 2484: 2468: 2439: 2432: 2423: 2407: 2401: 2378: 2358: 2338: 2336: 2316: 2293: 2273: 2255: 2237: 2231: 2207: 2201: 2175: 2160: 2134: 2121: 2114: 2105: 2083: 2077: 2054: 2048: 2028: 2004: 1982: 1960: 1938: 1896: 1864: 1845: 1835: 1824: 1814: 1803: 1791: 1765: 1740: 1715: 1692: 1686: 1664: 1630: 1612: 1605: 1599: 1578: 1558: 1537: 1525: 1507: 1500: 1488: 1475: 1457: 1450: 1435: 1417: 1410: 1408: 1366: 1342: 1322: 1294: 1266: 1265: 1253: 1243: 1228: 1222: 1200: 1180: 1160: 1125: 1119: 1098: 1092: 1071: 1065: 1040: 1031: 1020: 1011: 1000: 991: 989: 943: 938: 915: 904: 878: 866: 849: 842: 829: 821: 799: 778: 769: 693: 663: 634: 605: 576: 549: 527: 501: 475: 448: 442: 413: 386: 379: 370: 364: 5115:http://lindberglce.com/tech/buklbook.htm 4418:Super- and hypersonic aerospace vehicles 4025: 3932: 1708:, uniformly distributed compressive load 4484: 260:The ratio of the effective length of a 95: 4617: 4615: 4613: 4611: 4609: 4607: 4605: 711:is the effective length of the column. 4658:A general theory of elastic stability 4656:Thompson, J.M.T.; Hunt, G.W. (1973). 4584:SIAM Journal on Mathematical Analysis 4377:July 8, 2010 CSX train derailment in 4279:drivers, described as running over a 7: 5018:The Stability of Elastic Equilibrium 4466: – method in strucural analysis 3205:{\displaystyle \sigma L=\rho c^{2}h} 1337:is the acceleration due to gravity, 2837:is equal to 1. Tables of values of 268:of its cross section is called the 222:Buckling may occur even though the 4330:List of rail accidents (2000–2009) 3808: 3744: 3595: 3513: 2846:for simply supported beams exist. 1836: 1815: 1623: 1609: 1518: 1504: 1481: 1468: 1454: 1428: 1414: 74:or the wrinkling of a plate under 14: 5031:Journal of Structural Engineering 4008:Link model with transverse spring 3988:Link model with rotational spring 335:. He derived the formula, termed 4867:Robert C. Lauby (16 July 2012). 4423:deforms towards the flow-field. 5004:Journal of Aerospace Structures 4849:from the original on 2018-02-04 4785:Braun, Stephen (30 July 2002). 4439:Geometric and material buckling 4018:Link model with inclined spring 3694:Single-degree-of-freedom models 3274:is the elastic wave speed, and 2196:where the buckling coefficient 1361:of the beam cross section, and 542:, unsupported length of column, 54:is the sudden change in shape ( 4899:Journal of Sound and Vibration 4713:. CRC Press. p. 430-431. 4681:Magill, Bobby (31 July 2014). 4549:Ratzersdorfer, Julius (1936). 4328:more information available at 4255:Buckling is a failure mode in 4102: 4093: 3995:Unstable-symmetric bifurcation 3634: 3628: 3584: 3580: 3574: 3561: 3502: 3498: 3492: 3476: 3473: 3467: 2703:{\displaystyle b_{\text{eff}}} 1087:is the Euler maximum load and 875: 860: 730:The buckling load is directly 648:{\displaystyle K\approx 0.699} 566:column effective length factor 410: 400: 346:made of a homogeneous material 319:and the allowable compressive 1: 4845:. American University Radio. 3968:Stable-symmetric bifurcation 975:William John Macquorn Rankine 4997:(2nd ed.). McGraw-Hill. 4818:. Columbia, SC. 15 July 2010 4626:. Chatto and Windus, London. 4108:{\displaystyle P^{C}=c/(2L)} 3750:{\displaystyle V=U-P\Delta } 2777:, and the bottom side is in 4993:Theory of Elastic Stability 4734:Kim, Minho (17 July 2024). 4643:Martinus Nijhoff Publishers 3153:incomplete diagonal tension 2849:If an appropriate value of 2748:Flexural-torsional buckling 2732:{\displaystyle \sigma _{y}} 1195:, and cross-sectional area 926:{\displaystyle \sigma =F/A} 159:Metal-induced embrittlement 88:Johnson's parabolic formula 5166: 5060:Segui, Willian T. (2007). 4837:Lucero, Kat (2012-07-07). 4645:. pp. 11–56, 297–298. 4405:Pipes and pressure vessels 4214:{\displaystyle P^{C}=kL/2} 4162:{\displaystyle P^{C}=kL/2} 3254:is the length of the rod, 2783:lateral-torsional buckling 2757:Lateral-torsional buckling 1148: 961:is the slenderness ratio. 468:(vertical load on column), 149:Liquid metal embrittlement 66:, such as the bowing of a 25: 18: 4920:10.1016/j.jsv.2018.11.035 4869:Notice of Safety Advisory 4596:10.1137/s0036141097314537 3821:is the distance moved by 2997:{\displaystyle M_{\max }} 1679:, out-of-plane deflection 1381:is the first zero of the 1134:{\displaystyle F_{\max }} 349:free from initial stress. 164:Stress corrosion cracking 37:Buckled skin panels on a 21:Buckling (disambiguation) 5140:Mechanical failure modes 4390:West Hyattsville station 725:strength of the material 96:Mechanical failure modes 26:Not to be confused with 5088:Elishakoff, I. (2004). 5083:. Indianapolis: Jacobs. 4503:. Indianapolis: Jacobs. 4445:Perry–Robertson formula 3998:Asymmetric bifurcation 3887:saddle-node bifurcation 3814:{\displaystyle \Delta } 3307:{\displaystyle \sigma } 3227:{\displaystyle \sigma } 971:Perry Robertson formula 169:Sulfide stress cracking 5015:Koiter, W. T. (1945). 4989:; Gere, J. M. (1961). 4660:. London: John Wiley. 4639:Dynamic Pulse Buckling 4622:Bulson, P. S. (1970). 4388:train derailment near 4379:Waxhaw, North Carolina 4352:Crescent City, Florida 4300: 4295:Railway tracks in the 4221: 4215: 4169: 4163: 4115: 4109: 4057: 4041: 4019: 4009: 3989: 3979: 3954: 3875: 3855: 3835: 3815: 3791: 3771: 3751: 3716: 3700:total potential energy 3684: 3661: 3641: 3610: 3412: 3348: 3328: 3308: 3288: 3268: 3248: 3234:is the impact stress, 3228: 3206: 3085: 3056: 3027: 2998: 2966: 2766: 2733: 2704: 2672: 2553: 2533: 2511: 2387: 2367: 2347: 2325: 2303: 2220: 2219:{\displaystyle k_{cr}} 2188: 2064: 2037: 2013: 1991: 1969: 1947: 1922: 1840: 1819: 1774: 1749: 1724: 1702: 1673: 1648: 1375: 1351: 1331: 1309: 1209: 1189: 1169: 1135: 1108: 1081: 1052: 955: 927: 891: 808: 788: 787:{\displaystyle Ar^{2}} 752: 705: 678: 649: 620: 619:{\displaystyle K=0.50} 591: 558: 536: 518:area moment of inertia 510: 484: 464:, maximum or critical 458: 426: 257: 249: 139:Hydrogen embrittlement 48:structural engineering 43: 5079:Bruhn, E. F. (1973). 4624:Theory of Flat Plates 4499:Bruhn, E. F. (1973). 4433:Euler's critical load 4294: 4216: 4177: 4164: 4125: 4110: 4065: 4056: 4042: 4017: 4007: 3987: 3977: 3955: 3927:pitchfork bifurcation 3914:bifurcation; and the 3876: 3856: 3836: 3816: 3792: 3772: 3752: 3717: 3698:Using the concept of 3685: 3662: 3642: 3611: 3413: 3349: 3329: 3309: 3289: 3269: 3249: 3229: 3207: 3086: 3084:{\displaystyle M_{C}} 3057: 3055:{\displaystyle M_{B}} 3028: 3026:{\displaystyle M_{A}} 2999: 2967: 2773:, the top side is in 2764: 2734: 2705: 2673: 2554: 2534: 2512: 2388: 2368: 2348: 2326: 2304: 2221: 2189: 2065: 2063:{\displaystyle N_{x}} 2038: 2014: 1992: 1970: 1948: 1923: 1820: 1799: 1775: 1757:modulus of elasticity 1750: 1725: 1703: 1701:{\displaystyle N_{x}} 1674: 1649: 1376: 1359:second moment of area 1352: 1332: 1310: 1210: 1190: 1170: 1168:{\displaystyle \rho } 1136: 1109: 1107:{\displaystyle F_{c}} 1082: 1080:{\displaystyle F_{e}} 1053: 956: 928: 892: 809: 789: 749: 738:of the cross section. 736:second moment of area 706: 679: 677:{\displaystyle K=2.0} 650: 621: 600:For both ends fixed, 592: 590:{\displaystyle K=1.0} 559: 537: 511: 492:modulus of elasticity 485: 459: 457:{\displaystyle F_{c}} 427: 337:Euler's critical load 317:modulus of elasticity 255: 247: 84:Euler's critical load 36: 5130:Elasticity (physics) 4372:Kensington, Maryland 4299:affected by sun kink 4229:Engineering examples 4181: 4129: 4069: 4031: 3938: 3865: 3845: 3825: 3805: 3781: 3761: 3726: 3706: 3671: 3651: 3640:{\displaystyle w(x)} 3622: 3427: 3382: 3338: 3318: 3298: 3278: 3258: 3238: 3218: 3174: 3068: 3039: 3010: 2981: 2864: 2716: 2687: 2566: 2543: 2523: 2400: 2377: 2357: 2335: 2315: 2230: 2200: 2076: 2047: 2027: 2003: 1997:, length of specimen 1981: 1959: 1937: 1790: 1764: 1739: 1723:{\displaystyle \nu } 1714: 1685: 1663: 1407: 1365: 1341: 1321: 1221: 1199: 1179: 1159: 1118: 1091: 1064: 988: 937: 903: 820: 798: 768: 692: 662: 633: 604: 575: 548: 526: 500: 474: 441: 363: 60:structural component 19:For other uses, see 5145:Structural analysis 4960:2020AIAAJ..58.1423D 4911:2019JSV...443...74S 4710:Railway Geotechnics 4384:July 6, 2012 WMATA 4283:at highway speeds. 4048: 3961: 3953:{\displaystyle q=0} 2794:torsional stiffness 2346:{\displaystyle {b}} 2019:, width of specimen 954:{\displaystyle l/r} 154:Mechanical overload 4473:Yoshimura buckling 4319:(sleepers) along. 4309:expand when heated 4301: 4263:is more flexible. 4222: 4211: 4170: 4159: 4116: 4105: 4058: 4037: 4026: 4020: 4010: 3990: 3980: 3950: 3933: 3912:unstable-symmetric 3871: 3851: 3831: 3811: 3787: 3767: 3747: 3712: 3683:{\displaystyle xx} 3680: 3657: 3637: 3606: 3604: 3408: 3344: 3324: 3304: 3284: 3264: 3244: 3224: 3202: 3081: 3052: 3023: 2994: 2962: 2767: 2729: 2700: 2668: 2549: 2529: 2507: 2383: 2363: 2343: 2321: 2299: 2216: 2184: 2060: 2033: 2009: 1987: 1965: 1943: 1918: 1770: 1745: 1720: 1698: 1669: 1644: 1371: 1347: 1327: 1305: 1205: 1185: 1175:, Young's modulus 1165: 1131: 1104: 1077: 1048: 951: 923: 887: 804: 784: 753: 704:{\displaystyle KL} 701: 674: 645: 616: 587: 554: 532: 506: 480: 454: 422: 343:perfectly straight 266:radius of gyration 258: 250: 44: 5135:Materials science 5099:978-981-4583-53-4 5071:978-0-495-24471-4 5037:(10): 1253–1262. 4987:Timoshenko, S. P. 4969:10.2514/1.J059150 4791:Los Angeles Times 4580:C. Maeve McCarthy 4564:978-3-662-24075-5 4226: 4225: 4040:{\displaystyle P} 4024: 4023: 3904:bifurcation; the 3874:{\displaystyle V} 3854:{\displaystyle V} 3834:{\displaystyle P} 3790:{\displaystyle P} 3770:{\displaystyle U} 3715:{\displaystyle V} 3660:{\displaystyle x} 3556: 3550: 3531: 3459: 3441: 3405: 3392: 3347:{\displaystyle h} 3327:{\displaystyle h} 3287:{\displaystyle h} 3267:{\displaystyle c} 3247:{\displaystyle L} 2960: 2809:flexural strength 2739:, yielding stress 2710:, effective width 2697: 2666: 2659: 2658: 2616: 2584: 2578: 2552:{\displaystyle a} 2532:{\displaystyle b} 2505: 2492: 2386:{\displaystyle m} 2366:{\displaystyle m} 2324:{\displaystyle a} 2286: 2268: 2182: 2036:{\displaystyle n} 2012:{\displaystyle b} 1990:{\displaystyle a} 1968:{\displaystyle n} 1946:{\displaystyle m} 1912: 1880: 1773:{\displaystyle t} 1748:{\displaystyle E} 1672:{\displaystyle w} 1637: 1585: 1532: 1495: 1442: 1374:{\displaystyle B} 1350:{\displaystyle I} 1330:{\displaystyle g} 1302: 1287: 1263: 1231: 1208:{\displaystyle A} 1188:{\displaystyle E} 1046: 1026: 1006: 885: 837: 807:{\displaystyle I} 557:{\displaystyle K} 535:{\displaystyle L} 509:{\displaystyle I} 483:{\displaystyle E} 420: 277:center of gravity 270:slenderness ratio 235:Forms of buckling 220: 219: 114:Corrosion fatigue 5157: 5103: 5084: 5075: 5056: 5054: 5025: 5023: 5011: 4998: 4996: 4974: 4973: 4971: 4954:(4): 1423–1431. 4939: 4933: 4932: 4922: 4890: 4884: 4883: 4881: 4879: 4873: 4864: 4858: 4857: 4855: 4854: 4834: 4828: 4827: 4825: 4823: 4808: 4802: 4801: 4799: 4797: 4782: 4776: 4775: 4773: 4771: 4765: 4757: 4751: 4750: 4748: 4746: 4731: 4725: 4724: 4704: 4698: 4697: 4695: 4693: 4678: 4672: 4671: 4653: 4647: 4646: 4634: 4628: 4627: 4619: 4600: 4599: 4578:Cox, Steven J.; 4575: 4569: 4568: 4546: 4540: 4539: 4527: 4521: 4511: 4505: 4504: 4496: 4469: 4460: 4366:derailment, off 4346:derailment, off 4220: 4218: 4217: 4212: 4207: 4193: 4192: 4168: 4166: 4165: 4160: 4155: 4141: 4140: 4114: 4112: 4111: 4106: 4092: 4081: 4080: 4049: 4046: 4044: 4043: 4038: 3962: 3959: 3957: 3956: 3951: 3902:stable-symmetric 3880: 3878: 3877: 3872: 3860: 3858: 3857: 3852: 3840: 3838: 3837: 3832: 3820: 3818: 3817: 3812: 3796: 3794: 3793: 3788: 3776: 3774: 3773: 3768: 3756: 3754: 3753: 3748: 3721: 3719: 3718: 3713: 3689: 3687: 3686: 3681: 3666: 3664: 3663: 3658: 3646: 3644: 3643: 3638: 3615: 3613: 3612: 3607: 3605: 3598: 3592: 3591: 3573: 3572: 3557: 3552: 3551: 3548: 3542: 3533: 3532: 3529: 3516: 3510: 3509: 3491: 3490: 3460: 3452: 3443: 3442: 3439: 3417: 3415: 3414: 3409: 3407: 3406: 3403: 3394: 3393: 3390: 3353: 3351: 3350: 3345: 3333: 3331: 3330: 3325: 3313: 3311: 3310: 3305: 3293: 3291: 3290: 3285: 3273: 3271: 3270: 3265: 3253: 3251: 3250: 3245: 3233: 3231: 3230: 3225: 3211: 3209: 3208: 3203: 3198: 3197: 3163:Dynamic buckling 3130:diagonal tension 3123:Diagonal tension 3099:Plastic buckling 3090: 3088: 3087: 3082: 3080: 3079: 3061: 3059: 3058: 3053: 3051: 3050: 3032: 3030: 3029: 3024: 3022: 3021: 3003: 3001: 3000: 2995: 2993: 2992: 2971: 2969: 2968: 2963: 2961: 2959: 2958: 2957: 2942: 2941: 2926: 2925: 2910: 2909: 2896: 2895: 2894: 2881: 2876: 2875: 2738: 2736: 2735: 2730: 2728: 2727: 2709: 2707: 2706: 2701: 2699: 2698: 2695: 2677: 2675: 2674: 2669: 2667: 2665: 2661: 2660: 2657: 2656: 2647: 2646: 2634: 2633: 2617: 2615: 2614: 2605: 2604: 2592: 2590: 2585: 2580: 2579: 2576: 2570: 2558: 2556: 2555: 2550: 2538: 2536: 2535: 2530: 2516: 2514: 2513: 2508: 2506: 2504: 2503: 2502: 2497: 2493: 2485: 2478: 2474: 2473: 2472: 2448: 2444: 2443: 2433: 2431: 2430: 2415: 2414: 2392: 2390: 2389: 2384: 2372: 2370: 2369: 2364: 2352: 2350: 2349: 2344: 2342: 2330: 2328: 2327: 2322: 2308: 2306: 2305: 2300: 2298: 2297: 2292: 2288: 2287: 2285: 2274: 2269: 2264: 2256: 2245: 2244: 2225: 2223: 2222: 2217: 2215: 2214: 2193: 2191: 2190: 2185: 2183: 2181: 2180: 2179: 2170: 2166: 2165: 2164: 2140: 2139: 2138: 2126: 2125: 2115: 2113: 2112: 2097: 2096: 2069: 2067: 2066: 2061: 2059: 2058: 2042: 2040: 2039: 2034: 2018: 2016: 2015: 2010: 1996: 1994: 1993: 1988: 1974: 1972: 1971: 1966: 1952: 1950: 1949: 1944: 1927: 1925: 1924: 1919: 1917: 1913: 1908: 1897: 1885: 1881: 1876: 1865: 1853: 1852: 1839: 1834: 1818: 1813: 1779: 1777: 1776: 1771: 1754: 1752: 1751: 1746: 1729: 1727: 1726: 1721: 1707: 1705: 1704: 1699: 1697: 1696: 1678: 1676: 1675: 1670: 1653: 1651: 1650: 1645: 1643: 1639: 1638: 1636: 1635: 1634: 1621: 1617: 1616: 1606: 1604: 1603: 1586: 1584: 1583: 1582: 1569: 1568: 1564: 1563: 1562: 1538: 1533: 1531: 1530: 1529: 1516: 1512: 1511: 1501: 1496: 1494: 1493: 1492: 1480: 1479: 1466: 1462: 1461: 1451: 1443: 1441: 1440: 1439: 1426: 1422: 1421: 1411: 1380: 1378: 1377: 1372: 1356: 1354: 1353: 1348: 1336: 1334: 1333: 1328: 1314: 1312: 1311: 1306: 1304: 1303: 1295: 1293: 1289: 1288: 1286: 1275: 1267: 1264: 1259: 1258: 1257: 1244: 1233: 1232: 1229: 1214: 1212: 1211: 1206: 1194: 1192: 1191: 1186: 1174: 1172: 1171: 1166: 1140: 1138: 1137: 1132: 1130: 1129: 1113: 1111: 1110: 1105: 1103: 1102: 1086: 1084: 1083: 1078: 1076: 1075: 1057: 1055: 1054: 1049: 1047: 1045: 1044: 1032: 1027: 1025: 1024: 1012: 1007: 1005: 1004: 992: 960: 958: 957: 952: 947: 932: 930: 929: 924: 919: 896: 894: 893: 888: 886: 884: 883: 882: 870: 858: 854: 853: 843: 838: 830: 813: 811: 810: 805: 793: 791: 790: 785: 783: 782: 710: 708: 707: 702: 683: 681: 680: 675: 654: 652: 651: 646: 625: 623: 622: 617: 596: 594: 593: 588: 563: 561: 560: 555: 541: 539: 538: 533: 515: 513: 512: 507: 489: 487: 486: 481: 463: 461: 460: 455: 453: 452: 431: 429: 428: 423: 421: 419: 418: 417: 398: 391: 390: 380: 375: 374: 212: 205: 198: 93: 5165: 5164: 5160: 5159: 5158: 5156: 5155: 5154: 5120: 5119: 5110: 5100: 5087: 5078: 5072: 5059: 5028: 5021: 5014: 5001: 4985: 4982: 4980:Further reading 4977: 4941: 4940: 4936: 4892: 4891: 4887: 4877: 4875: 4871: 4866: 4865: 4861: 4852: 4850: 4836: 4835: 4831: 4821: 4819: 4810: 4809: 4805: 4795: 4793: 4784: 4783: 4779: 4769: 4767: 4763: 4759: 4758: 4754: 4744: 4742: 4733: 4732: 4728: 4721: 4706: 4705: 4701: 4691: 4689: 4687:Climate Central 4680: 4679: 4675: 4668: 4655: 4654: 4650: 4636: 4635: 4631: 4621: 4620: 4603: 4577: 4576: 4572: 4565: 4548: 4547: 4543: 4529: 4528: 4524: 4512: 4508: 4498: 4497: 4486: 4482: 4467: 4458: 4429: 4420: 4407: 4363:Capitol Limited 4337:April 18, 2002 4289: 4253: 4238:A conventional 4236: 4231: 4184: 4179: 4178: 4132: 4127: 4126: 4072: 4067: 4066: 4029: 4028: 3936: 3935: 3863: 3862: 3843: 3842: 3823: 3822: 3803: 3802: 3797:is the applied 3779: 3778: 3759: 3758: 3724: 3723: 3704: 3703: 3696: 3669: 3668: 3649: 3648: 3620: 3619: 3603: 3602: 3583: 3564: 3543: 3534: 3524: 3521: 3520: 3501: 3479: 3444: 3434: 3425: 3424: 3398: 3385: 3380: 3379: 3365: 3360: 3336: 3335: 3316: 3315: 3296: 3295: 3276: 3275: 3256: 3255: 3236: 3235: 3216: 3215: 3189: 3172: 3171: 3165: 3125: 3117: 3110: 3101: 3071: 3066: 3065: 3042: 3037: 3036: 3013: 3008: 3007: 2984: 2979: 2978: 2949: 2933: 2917: 2901: 2897: 2886: 2882: 2867: 2862: 2861: 2857: 2845: 2836: 2828: 2819: 2806: 2759: 2750: 2719: 2714: 2713: 2690: 2685: 2684: 2648: 2635: 2622: 2618: 2606: 2593: 2571: 2564: 2563: 2541: 2540: 2521: 2520: 2480: 2479: 2464: 2457: 2453: 2449: 2435: 2434: 2419: 2403: 2398: 2397: 2375: 2374: 2355: 2354: 2333: 2332: 2313: 2312: 2278: 2257: 2254: 2250: 2249: 2233: 2228: 2227: 2226:, is given by: 2203: 2198: 2197: 2171: 2156: 2149: 2145: 2141: 2130: 2117: 2116: 2101: 2079: 2074: 2073: 2050: 2045: 2044: 2025: 2024: 2001: 2000: 1979: 1978: 1957: 1956: 1935: 1934: 1898: 1892: 1866: 1860: 1841: 1788: 1787: 1762: 1761: 1737: 1736: 1732:Poisson's ratio 1712: 1711: 1688: 1683: 1682: 1661: 1660: 1626: 1622: 1608: 1607: 1595: 1591: 1587: 1574: 1570: 1554: 1547: 1543: 1539: 1521: 1517: 1503: 1502: 1484: 1471: 1467: 1453: 1452: 1431: 1427: 1413: 1412: 1405: 1404: 1391: 1383:Bessel function 1363: 1362: 1339: 1338: 1319: 1318: 1276: 1268: 1249: 1245: 1242: 1238: 1237: 1224: 1219: 1218: 1197: 1196: 1177: 1176: 1157: 1156: 1153: 1147: 1121: 1116: 1115: 1094: 1089: 1088: 1067: 1062: 1061: 1036: 1016: 996: 986: 985: 983: 935: 934: 901: 900: 874: 859: 845: 844: 818: 817: 796: 795: 774: 766: 765: 690: 689: 660: 659: 631: 630: 602: 601: 573: 572: 546: 545: 524: 523: 498: 497: 472: 471: 444: 439: 438: 409: 399: 382: 381: 366: 361: 360: 291:In particular: 242: 237: 216: 31: 24: 17: 12: 11: 5: 5163: 5161: 5153: 5152: 5147: 5142: 5137: 5132: 5122: 5121: 5118: 5117: 5109: 5108:External links 5106: 5105: 5104: 5098: 5085: 5076: 5070: 5057: 5026: 5012: 4999: 4981: 4978: 4976: 4975: 4934: 4885: 4859: 4829: 4803: 4777: 4752: 4740:New York Times 4726: 4719: 4699: 4673: 4666: 4648: 4629: 4601: 4590:(3): 547–554. 4570: 4563: 4541: 4522: 4506: 4483: 4481: 4478: 4477: 4476: 4470: 4461: 4452: 4450:Rail stressing 4447: 4442: 4436: 4428: 4425: 4419: 4416: 4406: 4403: 4398: 4397: 4382: 4375: 4357:July 29, 2002 4355: 4288: 4285: 4252: 4249: 4235: 4234:Bicycle wheels 4232: 4230: 4227: 4224: 4223: 4210: 4206: 4202: 4199: 4196: 4191: 4187: 4171: 4158: 4154: 4150: 4147: 4144: 4139: 4135: 4118: 4117: 4104: 4101: 4098: 4095: 4091: 4087: 4084: 4079: 4075: 4059: 4036: 4022: 4021: 4011: 4000: 3999: 3996: 3992: 3991: 3981: 3970: 3969: 3966: 3949: 3946: 3943: 3870: 3850: 3830: 3810: 3786: 3766: 3746: 3743: 3740: 3737: 3734: 3731: 3711: 3695: 3692: 3679: 3676: 3656: 3636: 3633: 3630: 3627: 3601: 3597: 3590: 3586: 3582: 3579: 3576: 3571: 3567: 3563: 3560: 3555: 3546: 3540: 3537: 3535: 3527: 3523: 3522: 3519: 3515: 3508: 3504: 3500: 3497: 3494: 3489: 3486: 3482: 3478: 3475: 3472: 3469: 3466: 3463: 3458: 3455: 3450: 3447: 3445: 3437: 3433: 3432: 3401: 3397: 3388: 3364: 3361: 3359: 3356: 3343: 3323: 3303: 3283: 3263: 3243: 3223: 3201: 3196: 3192: 3188: 3185: 3182: 3179: 3164: 3161: 3134:buckling ratio 3124: 3121: 3116: 3113: 3108: 3100: 3097: 3093: 3092: 3078: 3074: 3063: 3049: 3045: 3034: 3020: 3016: 3005: 2991: 2987: 2956: 2952: 2948: 2945: 2940: 2936: 2932: 2929: 2924: 2920: 2916: 2913: 2908: 2904: 2900: 2893: 2889: 2885: 2879: 2874: 2870: 2853: 2841: 2834: 2824: 2815: 2802: 2790:hollow section 2758: 2755: 2749: 2746: 2741: 2740: 2726: 2722: 2711: 2693: 2664: 2655: 2651: 2645: 2642: 2638: 2631: 2628: 2625: 2621: 2613: 2609: 2603: 2600: 2596: 2588: 2583: 2574: 2548: 2528: 2501: 2496: 2491: 2488: 2483: 2477: 2471: 2467: 2463: 2460: 2456: 2452: 2447: 2442: 2438: 2429: 2426: 2422: 2418: 2413: 2410: 2406: 2382: 2362: 2341: 2320: 2296: 2291: 2284: 2281: 2277: 2272: 2267: 2263: 2260: 2253: 2248: 2243: 2240: 2236: 2213: 2210: 2206: 2178: 2174: 2169: 2163: 2159: 2155: 2152: 2148: 2144: 2137: 2133: 2129: 2124: 2120: 2111: 2108: 2104: 2100: 2095: 2092: 2089: 2086: 2082: 2057: 2053: 2032: 2021: 2020: 2008: 1998: 1986: 1976: 1964: 1954: 1942: 1916: 1911: 1907: 1904: 1901: 1895: 1891: 1888: 1884: 1879: 1875: 1872: 1869: 1863: 1859: 1856: 1851: 1848: 1844: 1838: 1833: 1830: 1827: 1823: 1817: 1812: 1809: 1806: 1802: 1798: 1795: 1782: 1781: 1769: 1759: 1744: 1734: 1719: 1709: 1695: 1691: 1680: 1668: 1642: 1633: 1629: 1625: 1620: 1615: 1611: 1602: 1598: 1594: 1590: 1581: 1577: 1573: 1567: 1561: 1557: 1553: 1550: 1546: 1542: 1536: 1528: 1524: 1520: 1515: 1510: 1506: 1499: 1491: 1487: 1483: 1478: 1474: 1470: 1465: 1460: 1456: 1449: 1446: 1438: 1434: 1430: 1425: 1420: 1416: 1390: 1389:Plate buckling 1387: 1370: 1346: 1326: 1301: 1298: 1292: 1285: 1282: 1279: 1274: 1271: 1262: 1256: 1252: 1248: 1241: 1236: 1227: 1204: 1184: 1164: 1149:Main article: 1146: 1143: 1128: 1124: 1101: 1097: 1074: 1070: 1043: 1039: 1035: 1030: 1023: 1019: 1015: 1010: 1003: 999: 995: 981: 967:safety factors 950: 946: 942: 922: 918: 914: 911: 908: 881: 877: 873: 869: 865: 862: 857: 852: 848: 841: 836: 833: 828: 825: 803: 781: 777: 773: 744: 743: 739: 728: 713: 712: 700: 697: 687: 686: 685: 673: 670: 667: 656: 644: 641: 638: 627: 615: 612: 609: 598: 586: 583: 580: 553: 543: 531: 521: 505: 495: 479: 469: 451: 447: 416: 412: 408: 405: 402: 397: 394: 389: 385: 378: 373: 369: 351: 350: 347: 344: 333:Leonhard Euler 329: 328: 309: 301: 241: 238: 236: 233: 218: 217: 215: 214: 207: 200: 192: 189: 188: 187: 186: 181: 176: 171: 166: 161: 156: 151: 146: 141: 136: 131: 126: 121: 116: 111: 106: 98: 97: 15: 13: 10: 9: 6: 4: 3: 2: 5162: 5151: 5148: 5146: 5143: 5141: 5138: 5136: 5133: 5131: 5128: 5127: 5125: 5116: 5112: 5111: 5107: 5101: 5095: 5091: 5086: 5082: 5077: 5073: 5067: 5063: 5058: 5053: 5048: 5044: 5040: 5036: 5032: 5027: 5024:(PhD Thesis). 5020: 5019: 5013: 5009: 5005: 5000: 4995: 4994: 4988: 4984: 4983: 4979: 4970: 4965: 4961: 4957: 4953: 4949: 4945: 4938: 4935: 4930: 4926: 4921: 4916: 4912: 4908: 4904: 4900: 4896: 4889: 4886: 4870: 4863: 4860: 4848: 4844: 4840: 4833: 4830: 4817: 4813: 4807: 4804: 4792: 4788: 4781: 4778: 4762: 4756: 4753: 4741: 4737: 4730: 4727: 4722: 4716: 4712: 4711: 4703: 4700: 4688: 4684: 4677: 4674: 4669: 4667:9780471859918 4663: 4659: 4652: 4649: 4644: 4640: 4633: 4630: 4625: 4618: 4616: 4614: 4612: 4610: 4608: 4606: 4602: 4597: 4593: 4589: 4585: 4581: 4574: 4571: 4566: 4560: 4556: 4552: 4545: 4542: 4537: 4533: 4526: 4523: 4520: 4519:0-521-78210-4 4516: 4510: 4507: 4502: 4495: 4493: 4491: 4489: 4485: 4479: 4474: 4471: 4465: 4462: 4456: 4453: 4451: 4448: 4446: 4443: 4440: 4437: 4434: 4431: 4430: 4426: 4424: 4417: 4415: 4413: 4412:hoop stresses 4404: 4402: 4395: 4391: 4387: 4383: 4380: 4376: 4373: 4370:tracks, near 4369: 4365: 4364: 4360: 4356: 4353: 4350:tracks, near 4349: 4345: 4344: 4340: 4336: 4335: 4334: 4332: 4331: 4324: 4320: 4318: 4314: 4310: 4306: 4298: 4293: 4286: 4284: 4282: 4278: 4274: 4270: 4266: 4262: 4258: 4250: 4248: 4246: 4241: 4240:bicycle wheel 4233: 4228: 4208: 4204: 4200: 4197: 4194: 4189: 4185: 4176: 4172: 4156: 4152: 4148: 4145: 4142: 4137: 4133: 4124: 4120: 4119: 4099: 4096: 4089: 4085: 4082: 4077: 4073: 4064: 4060: 4055: 4051: 4050: 4034: 4016: 4012: 4006: 4002: 4001: 3997: 3994: 3993: 3986: 3982: 3976: 3972: 3971: 3967: 3964: 3963: 3947: 3944: 3941: 3931: 3929: 3928: 3923: 3919: 3918: 3917:transcritical 3913: 3909: 3908: 3903: 3899: 3898: 3897:supercritical 3893: 3889: 3888: 3882: 3868: 3848: 3828: 3800: 3784: 3764: 3741: 3738: 3735: 3732: 3729: 3709: 3701: 3693: 3691: 3677: 3674: 3654: 3631: 3625: 3616: 3599: 3588: 3577: 3569: 3565: 3558: 3553: 3544: 3538: 3536: 3525: 3517: 3506: 3495: 3487: 3484: 3480: 3470: 3464: 3461: 3456: 3453: 3448: 3446: 3435: 3422: 3418: 3399: 3395: 3386: 3377: 3373: 3369: 3363:Energy method 3362: 3357: 3355: 3341: 3321: 3301: 3281: 3261: 3241: 3221: 3212: 3199: 3194: 3190: 3186: 3183: 3180: 3177: 3169: 3162: 3160: 3156: 3154: 3149: 3145: 3143: 3139: 3135: 3131: 3122: 3120: 3114: 3112: 3105: 3098: 3096: 3076: 3072: 3064: 3047: 3043: 3035: 3018: 3014: 3006: 2985: 2977: 2976: 2975: 2972: 2954: 2950: 2946: 2943: 2938: 2934: 2930: 2927: 2922: 2918: 2914: 2911: 2902: 2898: 2887: 2883: 2877: 2872: 2868: 2859: 2856: 2852: 2847: 2844: 2840: 2832: 2827: 2823: 2818: 2814: 2810: 2805: 2801: 2797: 2795: 2791: 2786: 2784: 2780: 2776: 2772: 2763: 2756: 2754: 2747: 2745: 2724: 2720: 2712: 2691: 2683: 2682: 2681: 2678: 2662: 2653: 2649: 2643: 2640: 2636: 2629: 2626: 2623: 2619: 2611: 2607: 2601: 2598: 2594: 2586: 2581: 2572: 2561: 2546: 2526: 2517: 2499: 2494: 2489: 2486: 2481: 2475: 2469: 2465: 2461: 2458: 2454: 2450: 2445: 2440: 2436: 2427: 2424: 2420: 2416: 2411: 2408: 2404: 2394: 2380: 2360: 2339: 2318: 2309: 2294: 2289: 2282: 2279: 2275: 2270: 2265: 2261: 2258: 2251: 2246: 2241: 2238: 2234: 2211: 2208: 2204: 2194: 2176: 2172: 2167: 2161: 2157: 2153: 2150: 2146: 2142: 2135: 2131: 2127: 2122: 2118: 2109: 2106: 2102: 2098: 2093: 2090: 2087: 2084: 2080: 2071: 2055: 2051: 2030: 2006: 1999: 1984: 1977: 1962: 1955: 1940: 1933: 1932: 1931: 1928: 1914: 1909: 1905: 1902: 1899: 1893: 1889: 1886: 1882: 1877: 1873: 1870: 1867: 1861: 1857: 1854: 1849: 1846: 1842: 1831: 1828: 1825: 1821: 1810: 1807: 1804: 1800: 1796: 1793: 1785: 1767: 1760: 1758: 1742: 1735: 1733: 1717: 1710: 1693: 1689: 1681: 1666: 1659: 1658: 1657: 1654: 1640: 1631: 1627: 1618: 1613: 1600: 1596: 1592: 1588: 1579: 1575: 1571: 1565: 1559: 1555: 1551: 1548: 1544: 1540: 1534: 1526: 1522: 1513: 1508: 1497: 1489: 1485: 1476: 1472: 1463: 1458: 1447: 1444: 1436: 1432: 1423: 1418: 1402: 1399: 1396: 1388: 1386: 1384: 1368: 1360: 1344: 1324: 1315: 1299: 1296: 1290: 1283: 1280: 1277: 1272: 1269: 1260: 1254: 1250: 1246: 1239: 1234: 1225: 1216: 1202: 1182: 1162: 1152: 1151:Self-buckling 1145:Self-buckling 1144: 1142: 1122: 1099: 1095: 1072: 1068: 1058: 1041: 1037: 1033: 1028: 1021: 1017: 1013: 1008: 997: 993: 980: 976: 972: 968: 962: 948: 944: 940: 920: 916: 912: 909: 906: 897: 879: 871: 867: 863: 855: 850: 846: 839: 834: 831: 826: 823: 815: 801: 779: 775: 771: 761: 757: 748: 740: 737: 733: 729: 726: 722: 718: 717: 716: 698: 695: 688: 671: 668: 665: 657: 642: 639: 636: 628: 613: 610: 607: 599: 584: 581: 578: 570: 569: 567: 551: 544: 529: 522: 519: 503: 496: 493: 477: 470: 467: 449: 445: 437: 436: 435: 432: 414: 406: 403: 395: 392: 387: 383: 376: 371: 367: 358: 356: 348: 345: 342: 341: 340: 338: 334: 326: 322: 318: 313: 310: 306: 302: 298: 294: 293: 292: 289: 286: 282: 278: 273: 271: 267: 264:to the least 263: 254: 246: 239: 234: 232: 229: 225: 213: 208: 206: 201: 199: 194: 193: 191: 190: 185: 182: 180: 177: 175: 174:Thermal shock 172: 170: 167: 165: 162: 160: 157: 155: 152: 150: 147: 145: 142: 140: 137: 135: 132: 130: 127: 125: 122: 120: 117: 115: 112: 110: 107: 105: 102: 101: 100: 99: 94: 91: 89: 85: 81: 77: 73: 69: 65: 61: 57: 53: 49: 40: 35: 29: 22: 5089: 5080: 5062:Steel Design 5061: 5034: 5030: 5017: 5007: 5003: 4992: 4951: 4948:AIAA Journal 4947: 4937: 4902: 4898: 4888: 4876:. Retrieved 4862: 4851:. Retrieved 4842: 4832: 4820:. Retrieved 4815: 4806: 4794:. Retrieved 4790: 4780: 4768:. Retrieved 4755: 4743:. Retrieved 4739: 4729: 4709: 4702: 4690:. Retrieved 4686: 4676: 4657: 4651: 4638: 4632: 4623: 4587: 4583: 4573: 4554: 4550: 4544: 4535: 4531: 4525: 4509: 4500: 4421: 4408: 4401:incidents." 4399: 4361: 4341: 4327: 4325: 4321: 4312: 4302: 4265:Radiant heat 4254: 4237: 3925: 3921: 3915: 3911: 3905: 3901: 3895: 3891: 3885: 3883: 3799:conservative 3798: 3699: 3697: 3617: 3423: 3419: 3378: 3374: 3370: 3366: 3213: 3170: 3166: 3157: 3152: 3150: 3146: 3133: 3129: 3126: 3118: 3106: 3102: 3094: 2973: 2860: 2854: 2850: 2848: 2842: 2838: 2825: 2821: 2816: 2812: 2803: 2799: 2798: 2787: 2782: 2768: 2751: 2742: 2679: 2562: 2518: 2395: 2310: 2195: 2072: 2022: 1929: 1786: 1783: 1655: 1403: 1400: 1392: 1316: 1217: 1154: 1059: 978: 963: 898: 816: 762: 758: 754: 732:proportional 714: 516:, smallest 433: 359: 352: 330: 290: 274: 259: 221: 103: 79: 51: 45: 4464:Wood method 4305:rail tracks 4303:Similarly, 4297:Netherlands 4287:Rail tracks 3965:Limit Point 3907:subcritical 3892:limit point 2831:cantilevers 2775:compression 1780:, thickness 751:conditions. 355:equilibrium 72:compression 56:deformation 5124:Categories 5052:10092/4229 4853:2019-01-21 4720:148228880X 4480:References 4455:Stiffening 4343:Auto-Train 4281:speed hump 4277:automobile 3922:asymmetric 3368:analysis. 3144:failures. 2043:equals 1. 984:given by: 721:elasticity 285:deflection 5150:Mechanics 4929:125479249 4905:: 74–89. 4386:Metrorail 4267:from the 3809:Δ 3801:load and 3745:Δ 3739:− 3559:∫ 3462:∫ 3302:σ 3222:σ 3187:ρ 3178:σ 3115:Crippling 2721:σ 2650:σ 2637:σ 2627:− 2608:σ 2595:σ 2587:≈ 2466:ν 2462:− 2437:π 2405:σ 2158:ν 2154:− 2119:π 1903:π 1890:⁡ 1871:π 1858:⁡ 1837:∞ 1822:∑ 1816:∞ 1801:∑ 1718:ν 1624:∂ 1610:∂ 1593:− 1556:ν 1552:− 1519:∂ 1505:∂ 1482:∂ 1469:∂ 1455:∂ 1429:∂ 1415:∂ 1278:ρ 1163:ρ 907:σ 847:π 824:σ 640:≈ 384:π 288:bending. 109:Corrosion 4847:Archived 4427:See also 4394:Maryland 4313:sun kink 4257:pavement 3138:yielding 308:column). 305:concrete 303:A short 295:A short 224:stresses 184:Yielding 134:Fracture 104:Buckling 52:buckling 42:tension. 4956:Bibcode 4907:Bibcode 4878:18 July 4822:18 July 4796:18 July 4770:18 July 4745:18 July 4692:18 July 4261:asphalt 4245:pringle 3530:applied 3391:applied 3142:fatigue 2779:tension 2771:bending 1930:where 1357:is the 734:to the 325:species 240:Columns 228:failure 129:Fouling 124:Fatigue 80:buckled 58:) of a 5096:  5068:  4927:  4816:WIS 10 4717:  4664:  4561:  4517:  4359:Amtrak 4339:Amtrak 4273:expand 3894:; 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Index

Buckling (disambiguation)
buckle

B-52
structural engineering
deformation
structural component
load
column
compression
shear
Euler's critical load
Johnson's parabolic formula
Buckling
Corrosion
Corrosion fatigue
Creep
Fatigue
Fouling
Fracture
Hydrogen embrittlement
Impact
Liquid metal embrittlement
Mechanical overload
Metal-induced embrittlement
Stress corrosion cracking
Sulfide stress cracking
Thermal shock
Wear
Yielding

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