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CHARACTERISTICS OF FIVE EJECTOR CONFIGURATIONS AT FREE-STREAM MACH NUMBERS FROM 0 TO 2.0

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BookPublisher: Nasa, Washington, D.C. 1961Description: 41.DDC classification: NASA | TM X-23 -

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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-23 - (Browse shelf)	Not for loan Untraceable		TR9324

Total holds: 0

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Previous	NASA TM X-222 - STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5(DEGREE) SWEEPBACK & 45(DEGREE) DIHEDRAL AT A MACH NUMBER OF 6.2 & ANGLES OF ATTACK UP TO 20(DEGREE)	NASA TM X-226 - CONCEPT OF A MANNED SATELLITE REENTRY WHICH IS COMMPLETED WITH A GLIDE LANDING	NASA TM X-227 - LOW-SUBSONIC-SPEED STATIC LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A WINGED REENTRY-VEHICLE CONFIGURATION HAVING WINGTIP PANELS THAT FOLD UP FOR HIGH-DRAG REENTRY	NASA TM X-23 - CHARACTERISTICS OF FIVE EJECTOR CONFIGURATIONS AT FREE-STREAM MACH NUMBERS FROM 0 TO 2.0	NASA TM X-232 - HIGH-ALTITUDE PERFORMANCE OF A 64-FOOT-DIAMETER RING SAIL PARACHUTE	NASA TM X-233 - WIND-TUNNEL INVESTIGATION OF STATIC AERODYNAMIC CHARACTERISTICS OF A 1/9-SCALE MODEL OF A POSSIBLE REENTRY CAPSULE AT MACH NUMBERS FROM 2.29 TO 4.65	NASA TM X-235 - EXPERIMENTAL INVESTIGATION AND CORRELATION OF THE HEAT REDUCTION TO NONPOROUS SURFACES BEHIND A POROUS LEADING EDGE THROUGH WHICH COOLANT IS EJECTED	Next

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