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APPROXIMATE TEMPERATURE DISTRIBUTIONS AND STREAMWISE HEAT CONDUCTION EFFECTS IN THE TRANSIENT AERODYNAMIC HEATING OF THIN-SKINNED BODIES

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BookPublisher: Nasa, Washington, D.C. 1961Description: 90.DDC classification: NASA | TN D-895

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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-895 (Browse shelf)	Not for loan		TR16076

Total holds: 0

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Previous	NASA TN D-892 LOW-SUBSONIC MEASUREMENTS OF THE STATIC STABILITY AND CONTROL AND OSCILLATORY STABILITY DERIVATIVES OF A PROPOSED REENTRY VEHICLE HAVING AN EXTENSIBLE HEAT SHIELD FOR HIGH-DRAG REENTRY	NASA TN D-893 PRESSURE LOADS PRODUCED ON A FLAT-PLATE WING BY ROCKET JETS EXHAUSTING IN A SPANWISE DIRECTION BELOW THE WING AND PERPENDICULAR TO A FREE-STREAM FLOW OF MACH NUMBER 2.0	NASA TN D-894 INVESTIGATION OF LOW-SUBSONIC FLIGHT CHARACTERISTICS OF A MODEL OF A HYPERSONIC BOOST-GLIDE CONFIGURATION HAVING A 78(DEGRE) DELTA WING	NASA TN D-895 APPROXIMATE TEMPERATURE DISTRIBUTIONS AND STREAMWISE HEAT CONDUCTION EFFECTS IN THE TRANSIENT AERODYNAMIC HEATING OF THIN-SKINNED BODIES	NASA TN D-896 LOW-SPEED INVESTIGATION OF THE EFFECTS OF FREQUENCY AND AMPLITUDE OF OSCILLATION IN SIDESLIP ON THE LATERAL STABILITY DERIVATIVES OF A 60(DEGREE) DELTA WING, A 45(DEGRE) SWEPTBACK WING, AND AN - - -	NASA TN D-897 EXPLORATORY ENVIRONMENTAL TESTS OF SEVERAL HEAT SHIELDS	NASA TN D-898 REPEATABILITY OF THE OVER-ALL ERRORS OF AN AIRPLANE ALTIMETER INSTALLATION IN LANDING-APPROACH OPERATIONS	Next

Bound With Nasa Tn D-891-894,896-900

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