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DESIGN AND EVALUATION OF ACTIVE COOLING SYSTEM FOR MACH 6 CRUISE VEHICLE WINGS [NASA CR-1916]

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BookSeries: National Aeronautics and Space Administration(NASA). Publisher: Washington, D.C. NASA 1971Description: v, 267p.Subject(s): Equilibrium terperatures | Hypersonc heat loads | Hypersonic transportDDC classification: NASA | CR-1916

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1916 (Browse shelf)	Not for loan		TR8082

Total holds: 0

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Previous	NASA CR-1912 DEVELOPMENT AND APPLICATION OF A METHOD FOR PREDICTING ROTOR FREE WAKE POSITIONS AND RESULTING ROTOR BLADE AIR LOADS Volume II [NASA CR-1912)	NASA CR-1913 ANALYSIS OF FLIGHT DATA ON BOUNDARY LAYER TRANSITION AT HIGH ANGLES OF ATTACK[NASA CR 1913]	NASA CR-1914 A REVIEW OF THE OUTPUT PERFORMANCE OF SIX PLANAR THERMIONIC CONVERTERS WITH VARIOUS ELECTRODE MATERIALS [NASA CR-1914]	NASA CR-1916 DESIGN AND EVALUATION OF ACTIVE COOLING SYSTEM FOR MACH 6 CRUISE VEHICLE WINGS [NASA CR-1916]	NASA CR-1917 EVALUATION OF ACTIVE COOLING SYSTEM FOR A MACH 6 HYPERSONIC TRANSPORT AIRFRAME [NASA CR-1917]	NASA CR-1918 DESIGN OF A CONVECTIVE COOLING SYSTEM FOR A MACH 6 HYPERSONIC TRANSPORT AIRFRAME [NASA CR-1918]	NASA CR-1919 UNIVERSITY ROLE IN ASTRONAUT LIFE SUPPORT SYSTEM [NASA CR1919]	Next

Bound With NASA CR-1911-19(Bound With Acc No. 101559)

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