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HEATING AND FLOW-FIELD STUDIES ON A STRAIGHT-WING HYPERSONIC REENTRY VEHICLE AT ANGLES OF ATTACK FROM 20[DEGREE] TO 80[DEGREE] WITH SIMULATION OF REAL-GAS TRENDS

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BookPublisher: Nasa, Washington, D.C. 1973Description: 94.DDC classification: NASA | TN D-7108 -

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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 TN D-7108 - (Browse shelf)	Not for loan		TR9739

Total holds: 0

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Previous	NASA TN D-7105 - NONLINEAR THEORY FOR SONIC-BOOM CALCULATIONS IN A STRATIFIED ATMOSPHERE	NASA TN D-7106 - TAKEOFF CERTIFICATION CONSIDERATIONS FOR LARGE SUBSONIC AND SUPERSONIC TRANSPORT AIRPLANES USING THE AMES FLIGHT SIMULATOR FOR ADVANCED AIRCRAFT	NASA TN D-7107 - MIXED FINITE-DIFFERENCE SCHEME FOR FREE-VIBRATION ANALYSIS OF NONCIRCULAR CYLINDERS	NASA TN D-7108 - HEATING AND FLOW-FIELD STUDIES ON A STRAIGHT-WING HYPERSONIC REENTRY VEHICLE AT ANGLES OF ATTACK FROM 20[DEGREE] TO 80[DEGREE] WITH SIMULATION OF REAL-GAS TRENDS	NASA TN D-7109 - EFFECT OF REYNOLDS NUMBER AND ENGINE NACELLES ON THE STALLING CHARACTERISTICS OF A MODEL OF A TWIN-ENGINE LIGHT AIRPLANE	NASA TN D-711 INVESTIGATION OF THE STATIC LONGITUDINAL AND LATERAL STABILITY CHARACTERISTICS OF A 0.10-SCALE MODEL OF A THREE-STAGE CONFIGURATION OF THE SCOUT RESEARCH VEHICLE AT MACH NUMBERS OF 2.29, 2.96, 3.96	NASA TN D-7111 APOLLO EXPERIENCE REPORT - THE PROBLEM OF STRESS-CORROSION CRACKING	Next

Bound With Nasa Tn D-7100-09

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