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SPIN-ENTRY CHRACTERISTICS OF A DELTA-WING AIRPLANE AS DETRMINED BY A DYNAMIC MODEL.

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BookPublisher: Nasa, Washington, D.C. 1965Description: 50.DDC classification: NASA | TN D-2656

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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-2656 (Browse shelf)	Not for loan		TR16104

Total holds: 0

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Previous	NASA TN D-2653 AN EXPERIMENTAL INVESTIGATION OF PEAK AND AERAGE HEATING EFFECTS IN CASCADE JETS.	NASA TN D-2654 A MODIFIED METHOD OF INTEGERAL RELATION FOR SUPERSONIC NONEQUILIBRIUM FLOW OVER A WEDGE	NASA TN D-2655 TRIM REQUIREMENTS AND STATIC-STABILITY DERVATIVES FROM A WIND-TUNNEL INVESTIGATION OF A LIFTING ROTOR IN TRANSITION	NASA TN D-2656 SPIN-ENTRY CHRACTERISTICS OF A DELTA-WING AIRPLANE AS DETRMINED BY A DYNAMIC MODEL.	NASA TN D-2657 POSSIBLE PROTON-ALPHA SCATTERING EXPERIMENTS AT 40 MEV	NASA TN D-2658 BEHAVIOR OF LIQUID-VAPOR INTERFACE OF CRYOGENIC LIQUIDS DURING WEIGHTLESSNESS.	NASA TN D-2659 ELECTRON-BREMSSTRAHLUNG DIFFERENTIAL CROSS SECTIONS FOR THIN AND THICK TARGETS	Next

Bound With Nasa Tn D-2651-2655,2657-2660.

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