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EXPERIMENTAL AND CALCULATED FLOW FIELDS PRODUCED BY AIRPLANES FLYING AT SUPERSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1960Description: 24.DDC classification: NASA | TN D-621

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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-621 (Browse shelf)	Not for loan		65474

Total holds: 0

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Previous	NASA TN D-6207 - ENERGY TRANSFER RATES OF AN INTEGRATED LIFE SUPPORT SYSTEM DURING MANNED AND INTERMITTENTLY MANNED TESTS	NASA TN D-6208 - EXPERIENCE WITH THE X-15 ADAPTIVE FLIGHT CONTROL SYSTEM	NASA TN D-6209 - VARIANCE REDUCTION BY IMPROTANCE SAMPLING AND THE METHOD OF SPLITING IN MONTE CARLO CALCULATIONS	NASA TN D-621 EXPERIMENTAL AND CALCULATED FLOW FIELDS PRODUCED BY AIRPLANES FLYING AT SUPERSONIC SPEEDS	NASA TN D-6210 - FLIGHT EVALUATION OF ANGLE OF ATTACK AS A CONTROL PARAMETER IN GENERAL-AVIATION AIRCRAFT	NASA TN D-6211 - EFFECT OF HYDROGEN ON TENSILE PROPERTIES OF PALLADIUM-HYDROGEN SYSTEM	NASA TN D-6212 - TWO-PHASE HYDROGEN DENSITY MEASUREMENTS USING AN OPEN-ENDED MICROWAVE CAVITY	Next

Bound With Nasa Tn D-622-630

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