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APPROXIMATE CALCULATION OF HYPERSONIC CONICAL FLOW PARAMETERS FOR AIR IN THERMODYNAMICS EQUILIBRIUM.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 15.DDC classification: NASA | TN D-2058

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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-2058 (Browse shelf)	Not for loan		TR15582

Total holds: 0

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Previous	NASA TN D-2055 STUDY OF THE USE OF TERMINAL CONTROL TECHNIQUES FOR GUIDENCE DURING DIRECT AND SKIP ENTRIES FOR A CAPSULE-TYPE VEHICLE AT PARABOLIC VELOCITY.	NASA TN D-2056 PHENOMENA OF PNEUMATIC TIRE HYDROPLANNING.	NASA TN D-2057 STATIC LONGITUDINAL CHRACTERISTICS OF THE PROJECT FIRE REENTRY STAGE AFTER REENTRY-PACKAGE SEPRATION AT MACH 28.3 IN HELIUM.	NASA TN D-2058 APPROXIMATE CALCULATION OF HYPERSONIC CONICAL FLOW PARAMETERS FOR AIR IN THERMODYNAMICS EQUILIBRIUM.	NASA TN D-2059 IMPORTANT STRUCTURAL RESEARCH PROBLEMS FOR THE SUPPORT OF FUTURE SPACE MISSIONS.	NASA TN D-206 HETEROGENEOUS COMBUSTION OF MULTICOMPONENT FUELS	NASA TN D-2060 A PILOTED SIMULATOR STUDY OF THE LOSS OF ALTITUDE BY JET TRANSPORT IN A GO-AROUND FROM AN INSTRUMENT-LANDING APPOACH.	Next

Bound With Nasa Tn D-2051-2057,2059-2060.

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