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Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at mach numbers from 0.65 to 10.6

By: Walter P Nelms,Jr.

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BookPublisher: Description: v.DDC classification: NASA | TN D-6821 -

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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-6821 - (Browse shelf)	Not for loan		TR9819

Total holds: 0

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Previous	NASA TN D-6818 - CALCULATION OF LINEARIZED SUPERSONIC FLOW OVER SLENDER CONES OF ARBITRARY CROSS SECTION	NASA TN D-6819 - VERSATILE MOSSBAUER SPECTROMETER AND ITS APPLICATIONS IN VIBRATION MEASUREMENT	NASA TN D-682 THEORETICAL PERFORMANCE OF PROPELLANTS SUITABLE FOR ELECTROTHERMAL JET ENGINES	NASA TN D-6821 - Effects of body shape on the aerodynamic characteristics of an all-body hypersonic aircraft configuration at mach numbers from 0.65 to 10.6	NASA TN D-6822 - Surface-refractivity measurements at NASA spacecraft tracking sites	NASA TN D-6823 - Sonic-boom measurements for SR-71 aircraft operating at mach numbers to 3.0 and altitudes to 24384 meters	NASA TN D-6824 - Experimental findings from zero-tank net positive suction head operation of the J-2 hydrogen pump	Next

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