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LAMINAR HEAT-TRANSFER AND PRESSURE-DISTRIBUTION STUDIES ON A SERIES OF REENTRY NOSE SHAPES AT A MACH NUMBER OF 19.4 IN HELIUM

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BookPublisher: Nasa, Washington, D.C. 1961Description: 39.DDC classification: NASA | TN D-891

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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-891 (Browse shelf)	Not for loan		65490

Total holds: 0

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Previous	NASA TN D-868 EXPERIMENTAL INVESTIGATION OF STAGE SEPARATION AERODYNAMICS.	NASA TN D-869 TURBULENT SKIN-FRICTION AND HEAT-TRANSFER COEFFICIENTS FOR AN INCLINED FLAT PLATE AT HIGH HYPERSONIC SPEEDS IN TERMS OF FREE-STREAM FLOW PROPERTIES.	NASA TN D-870 A COOLED-TUBE PYROMETER WITH EXPERIMENTAL RESULTS OBTAINED IN A HIGH-TEMPERATURE GAS STREAMS .	NASA TN D-891 LAMINAR HEAT-TRANSFER AND PRESSURE-DISTRIBUTION STUDIES ON A SERIES OF REENTRY NOSE SHAPES AT A MACH NUMBER OF 19.4 IN HELIUM	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	Next

Bound With Nasa Tn D-892-900

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