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STATIC STABILITY CHARACTERISTICS OF A SERIES OF HYPERSONIC BOOST-GLIDE CONFIGURATIONS AT MACH NUMBERS OF 1.41 AND 2.01

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BookPublisher: Nasa, Washington, D.C. 1959Description: 85.DDC classification: NASA | TM X-167 -

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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-167 - (Browse shelf)	Not for loan Untraceable		TR8832

Total holds: 0

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Previous	NASA TM X-154 PERFORMANCE OF A MACH NUMBER 3.0 DESIGN AXISYMMETRIC DOUBLE-CONE EXTERNAL-COMPRESSION INLET IN THE MACH NUMBER RANGE 1.97 TO 0.79	NASA TM X-156 AN EXPERIMENTAL INVESTIGATION AT MACH NUMBERS FROM 2.1 TO 3.0 OF CIRCULAR INTERNAL-COMPRESSION INLETS HAVING TRANSLATABLE CENTERBODIES AND PROVISIONS FOR BOUNDARY-LAYER REMOVAL	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	Next

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