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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

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BookPublisher: Nasa, Washington, D.C. 1960Description: 39.DDC classification: NASA | TM X-172 -

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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-172 - (Browse shelf)	Not for loan Untraceable		TR8834

Total holds: 0

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Previous	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	NASA TM X-183 USE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT OR UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS	Next

Bound With Nasa Tm X-165-79

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