FR1484155A - Perfectionnements apportés aux canons à grande vitesse, notamment pour la mesure de la résistance au choc d'un aéronef contre des êtres ailés
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Perfectionnements apportés aux canons à grande vitesse, notamment pour la mesure de la résistance au choc d'un aéronef contre des êtres ailés
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Fiat SpA
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B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
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Aviation & Aerospace Engineering
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FR66149A1965-06-211966-06-20Perfectionnements apportés aux canons à grande vitesse, notamment pour la mesure de la résistance au choc d'un aéronef contre des êtres ailés
ExpiredFR1484155A
(fr)
Dynamic stability testing with ablation at mach 14 in a long duration wind tunnel(Hypersonic blowdown wind tunnel testing of the dynamic stability of ablating nose cones)
Experimental procedure, the simulator, and the evaluation criteria used to determine the effects of the coefficient of the angle of attack and true speed on the longitudinal handling qualities of supersonic transports
Determination of the flow upstream of a hemispherical obstacle placed at zero incidence in a current of a perfect fluid at supersonic speed(Flow characteristics behind detached shock wave of hemispherical obstacle placed at zero incidence in current of perfect fluid at supersonic speed)
Uniform plane mhd shock traveling with constant speed into an ideal, perfectly conducting fluid at rest in a channel which has a section of nonuniform area