26:
244:
151:
Originally designed to produce 1,000 hp (746 kW) the
Mistral never achieved the required power output and the H.V.40 did not fly until July 1931. The first flight was from Lake Berre the base of the French team for the 1931 race. The H.V.40 flew well but had poor high-speed performance and
144:
landplane fighter. It was a streamlined single-seat cantilever monoplane and had two metal floats attached underneath the fuselage on inverted vee-struts. The H.V.40 was to powered by a
148:
radial engine. The aircraft was ready for testing by May 1929 but due to delays with the engine it did not fly and the French government withdrew the team from the 1929 race.
412:
362:
Meurillon, Louis (August 1976). "La Coupe
Schneider et la Société des Avions Bernard (2)" [The Schneider Cup and the Bernard Company, Part 2].
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were two designs ordered for use by the French team in the 1929
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347:. Collection Docavia. Vol. 31. Paris: Éditions Larivière.
231:
420 km/h (261 mph, 227 kn) (estimated)
531:
460:
429:
116:for the French government to compete in the 1929
216:radial piston engine , 597 kW (800 hp)
152:was only used for a number of training flights.
406:
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206:10.00 m (107.64 sq ft)
200:3.60 m (11 ft 9.75 in)
188:7.41 m (24 ft 3.75 in)
7:
382:Illustrated Encyclopedia of Aircraft
287:List of flying boats and floatplanes
194:8.70 m (28 ft 6.5 in)
166:Illustrated Encyclopedia of Aircraft
14:
242:
24:
800:Single-engined tractor aircraft
1:
136:. The H.V.40 was designed by
810:Aircraft first flown in 1931
780:1930s French sport aircraft
826:
114:Société des Avions Bernard
66:Société des Avions Bernard
23:
18:
214:Gnome-Rhône 9Kfr Mistral
146:Gnome-Rhône 9Kfr Mistral
366:(in French) (81): 3–7.
173:General characteristics
140:and was similar to the
124:Design and development
384:(Part Work 1982-1985)
364:Le Fana de l'Aviation
343:Liron, Jean (1990).
386:. Orbis Publishing.
264:Related development
345:Les avions Bernard
329:Orbis 1985, p. 653
805:Low-wing aircraft
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795:Bernard aircraft
785:Schneider Trophy
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258:Schneider Trophy
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134:Schneider Trophy
118:Schneider Trophy
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44:Type of aircraft
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430:Adolphe Bernard
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250:Aviation portal
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128:The H.V.40 and
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51:National origin
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19:Bernard H.V.40
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229:Maximum speed:
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156:Specifications
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138:Georges Bruner
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103:Bernard H.V.40
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281:Related lists
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112:designed by
102:
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91:Number built
36:Single-seat
790:Floatplanes
222:Performance
210:Powerplant:
774:Categories
293:References
204:Wing area:
142:Bernard 20
372:0757-4169
192:Wingspan:
161:Data from
72:Designer
554:18 T Bis
461:S.I.M.B.
424:aircraft
236:See also
110:seaplane
41:seaplane
569:191 GR
422:Bernard
198:Height:
186:Length:
749:HV 320
739:HV 220
719:200 TS
699:HV 120
619:H.V.42
614:H.V.41
609:H.V.40
594:197 GR
549:181 GR
532:S.A.B.
503:AB 10T
370:
351:
130:H.V.41
107:racing
105:was a
56:France
38:racing
754:510 T
734:207 T
729:205 T
724:201 T
714:200 T
694:H 110
684:84 GR
674:81 GR
669:80 GR
589:195 T
584:194 T
579:193 T
574:192 T
564:191 T
559:190 T
544:18 GR
523:AB 16
518:AB 15
513:AB 14
508:AB 12
498:AB 10
478:AB 3T
473:AB 3M
468:AB.C1
298:Notes
180:Crew:
85:1931
33:Role
659:74 S
654:S-73
649:S-72
634:61 T
629:60 T
624:H.52
604:30 T
539:18 T
452:AB 4
447:AB 3
442:AB 2
437:AB 1
380:The
368:ISSN
349:ISBN
212:1 ×
164:The
101:The
759:V.4
744:260
709:161
704:160
493:V.3
488:V.2
483:V.1
776::
689:86
679:82
664:75
644:71
639:70
599:20
306:^
120:.
95:1
414:e
407:t
400:v
374:.
357:.
182:1
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
