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AN INVESTIGATION OF A 0.05-SCALE MODEL OF THE XSM-64A NAVAHO MISSILE AND BOOSTER AT SUPERSONIC MACH NUMBERS PART II-PRESSURE STUDY

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BookPublisher: Nasa, Washington, D.C. 1959Description: 136.DDC classification: NASA | TM X-17

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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-17 (Browse shelf)	Not for loan		TR16269

Total holds: 0

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Previous	NASA TM X-16 AN INVESTIGATION OF A 0.05-SCALE MODEL OF THE XSM-64A NAVAHO MISSILE AND BOOSTER AT SUPERSONIC MACH NUMBERS	NASA TM X-167 - STATIC STABILITY CHARACTERISTICS OF A SERIES OF HYPERSONIC BOOST-GLIDE CONFIGURATIONS AT MACH NUMBERS OF 1.41 AND 2.01	NASA TM X-169 - OBSERVATIONS ON THE FLOWS PAST BLUNT BODIES AT TRANSONIC SPEEDS	NASA TM X-17 AN INVESTIGATION OF A 0.05-SCALE MODEL OF THE XSM-64A NAVAHO MISSILE AND BOOSTER AT SUPERSONIC MACH NUMBERS PART II-PRESSURE STUDY	NASA TM X-172 - AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS OF 1.41 AND 2.01 OF A SERIES OF CRANKED WINGS RANGING IN ASPECT RATIO FROM 4.00 TO 1.74 IN COMBINATION WITH A BODY	NASA TM X-178 - EXPLORATORY INVESTIGATION AT MACH NUMBER OF 2.01 OF THE LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION	NASA TM X-179 - WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE	Next

Bound With Nasa Tm X-5-16,19, Lack No. 6-7,10-15,18

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