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TRANSONIC AND SUPERSONIC WIND-TUNNEL TESTS OF WING-BODY COMBINATIONS DESIGNED FOR HIGH EFFICIENCY AT A MACH NUMBER OF 1.41

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BookPublisher: Nasa, Washington, D.C. 1960Description: 82.DDC classification: NASA | TN D-435

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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-435 (Browse shelf)	Not for loan		TR15848

Total holds: 0

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Previous	NASA TN D-434 LOW-SPEED INVESTIGATION OF A FULL-SPAN INTERNAL-FLOW JET-AUGMENTED FLAP ON A HIGH-WING MODEL WITH A 35 DEGREE WING OF ASPECT RATIO7.0	NASA TN D-4340 EFFECTS OF WALL PRESSURE DISTRIBUTION AND LIQUID TEMPERATURE ON INCIPIENT CAVITATION OF FREON-114 AND WATER IN VENTURI FLOW	NASA TN D-4347 DEVELOPMENT AND APPLICATION OF A LOCAL LINEARIZATION ALGORAITHM FOR THE INTGERIZATION OF QUATERNION RATE EQUATIONS IN REAL-TIME FLIGHT SIMULATION PROBLEMS.	NASA TN D-435 TRANSONIC AND SUPERSONIC WIND-TUNNEL TESTS OF WING-BODY COMBINATIONS DESIGNED FOR HIGH EFFICIENCY AT A MACH NUMBER OF 1.41	NASA TN D-4352 METHOD FOR CALCULATING ALLOWABLE CREEP STRESS IN LINEARLY INCREASING STRESS ENVIRONMENT.	NASA TN D-4353 TRANSIENT SOLIDFICATION OF A FLOWING LIQUID A COLD PLATE INCLUDING HEAT CAPACITIES OF FROZEN LAYER AND PLATE.	NASA TN D-4354 AN UNCERTAINTY ANALYSIS FOR SATELLITE CALORIMETRIC MEASUREMENTS.	Next

Bound With Nasa Tn D-431-34,436-40

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