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CONSTANT DENSITY APPROXIMATIONS FOR THE FLOW BEHIND AXISYMMETRIC SHOCK WAVES

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BookPublisher: Nasa, Washington, D.C. 1961Description: 29.DDC classification: NASA | TN D-857

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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-857 (Browse shelf)	Not for loan		TR16059

Total holds: 0

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Previous	NASA TN D-854 INVESTIGATION OF AN AXISYMMETRIC INTERNAL COMPRESSION INLET AT A MACH NUMBER OF ABOUT 3.8	NASA TN D-855 A STUDY OF LAMINAR COMPRESSIBLE VISCOUS PIPE FLOW ACCELERATED BY AN AXIAL BODY FORCE, WITH APPLICATION TO MAGNETOGASDYNAMICS	NASA TN D-856 EXPERIMENTAL EVALUATION OF ANALYTICAL MODELS FOR THE INERTIAS AND NATURAL FREQUENCIES OF FUEL SLOSHING IN CIRCULAR CYLINDRICAL TANKS	NASA TN D-857 CONSTANT DENSITY APPROXIMATIONS FOR THE FLOW BEHIND AXISYMMETRIC SHOCK WAVES	NASA TN D-858 DESIGN AND FLIGHT TESTS OF AN ADAPTIVE CONTROL SYSTEM EMPLOYING NORMAL-ACCELERATION COMMAND	NASA TN D-859 UNSTEADY AERODYNAMIC FORCES ON A SLENDER BODY OF REVOLUTION IN SUPERSONIC FLOW	NASA TN D-860 PREDICTED SHOCK ENVELOPES ABOUT TWO TYPES OF VEHICLES AT LARGE ANGLES OF ATTACK	Next

Bound With Nasa Tn D-851-856,858-860

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