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INVESTIGATION OF AN AXISYMMETRIC INTERNAL COMPRESSION INLET AT A MACH NUMBER OF ABOUT 3.8

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BookPublisher: Nasa, Washington, D.C. 1961Description: 31.DDC classification: NASA | TN D-854

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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-854 (Browse shelf)	Not for loan		TR16056

Total holds: 0

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Previous	NASA TN D-810 TOLERABLE LIMITS OF OSCILLATORY ACCELERATIONS DUE TO ROLLING MOTIONS EXPERIENCED BY ONE PILOT DURING AUTOMATIC-INTERCEPTOR FLIGHT TESTS	NASA TN D-852 A PRELIMINARY STUDY OF THE AGOUSTIC TRANSMISSION LOSS OF TWO FIBERGLAS NOSE -CONE SHAPES	NASA TN D-853 AN INVESTIGATION OF TRANSONIC FLOW FIELDS SURROUNDING HOT AND COLD SONIC JETS	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	Next

Bound With Nasa Tn D-851-853,855-860

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