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STABILITY AND CONTRL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

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BookPublisher: Nasa, Washington, D.C. 1961Description: 27.DDC classification: NASA | TM X-441

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TM X-441 (Browse shelf)	Not for loan		TR11662

Total holds: 0

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Previous	NASA TM X-437 FREE-FLIGHT TESTS TO A MACH NUMBER OF 1.5 OF SLENDER TRANGULAR PYRAMID REENTRY CONFIGURATIONS	NASA TM X-439 THE EFFECT OF AIR BLEED ON THE HEAT TRANSFER AND PRESSURE DISTRIBUTION ON 30 DEGREE C CONICAL FLARES AT A MACH NUMBER OF 6.8	NASA TM X-440 AN INVESTIGATION AT SUBSONIC SPEEDS OF THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM-4 DEGREE TO 100 DEGREE OF DELTA-WING REENTRY CONFIGURATIONS HAVING VERTICALLY DISPLACED ...	NASA TM X-441 STABILITY AND CONTRL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS	NASA TM X-449 EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEGREE	NASA TM X-459 DYNAMIC MODEL TESTS AT LOW SUBSONIC SPEEDS OF PROJECT MERCURY CAPSULE CONFIGURATIONS WITH AND WITHOUT DROGUE PARACHUTES	NASA TM X-467 INVESTIGATION OF THE NORMAL-FORCE, AXIAL-FORCE, AND PITCHING-MOMENT CHARACTERISTICS OF BLUNT LOW-FINENESS-RATIO BODIES OF REVOLUTION AT A MACH NUMBER OF 3.55	Next

Bound With Nasa Tm X-416-40,448-79 Lack No.418-22,24,26,28-29,32,34-36,38,42-47,50-58,60-66,69-78

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