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CALCULATION OF LINEARIZED SUPERSONIC FLOW OVER SLENDER CONES OF ARBITRARY CROSS SECTION

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BookPublisher: Nasa, Washington, D.C. 1972Description: 39.DDC classification: NASA | TN D-6818 -

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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-6818 - (Browse shelf)	Not for loan		TR8140

Total holds: 0

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Previous	NASA TN D-6815 - SENSITIVITY OF HOT-CATHODE IONIZATION VACUUM GAGES IN SEVERAL GAGES	NASA TN D-6816 - EXPERIMENTAL STATIC AERODYNAMICS OF A REGULAR HEXAGONAL PRISM IN A LOW-DENSITY HYPERVELOCITY FLOW	NASA TN D-6817 - NORMAL IMPINGEMENT LOADS DUE TO SMALL AIR JETS ISSUING FROM A BASE PLATE AND REFLECTING OFF A PLATFORM FOR VARIOUS JET MACH NUMBERS, SEPARATION DISTANCES, AND AMBIENT PRESSURES	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	Next

Bound With Nasa Tn D-6801-19

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