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SECONDARY FLOW FIELDS EMBEDDED IN HYPERSONIC SHOCK LAYERS

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BookPublisher: Nasa,Washington, D.C. 1962Description: 23.DDC classification: NASA | TN D-1304 -

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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-1304 - (Browse shelf)	Not for loan		TR9659

Total holds: 0

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Previous	NASA TN D-1300 EFFECTS OF SIMULATED RETROROCKETS ON THE AERODYNAMIC CHARACTERISTICS OF A BODY OF REVOLUTION AT MACH NUMBERS FROM 0.25 TO 1.90	NASA TN D-1302 - MEASURED STEADY-STATE PERFORMANCE OF WATER VAPOR JETS FOR USE IN SPACE VEHICLE ATTITUDE CONTROL SYSTEM	NASA TN D-1303 - APPROXIMATIONS FOR THE THERMODYNAMIC AND TRANSPORT PROPERTIES OF HIGH-TEMPERATURE NITROGEN WITH SHOCK-TUBE APPLICATIONS	NASA TN D-1304 - SECONDARY FLOW FIELDS EMBEDDED IN HYPERSONIC SHOCK LAYERS	NASA TN D-1305 - EMISSION SPECTRA FROM HIGH-PRESSURE HYDROGEN-OXYGEN COMBUSTION	NASA TN D-1308 - SURVEY OF ENERGY-ABSORPTION DEVICES FOR SOFT LANDING OF SPACE VEHICLES	NASA TN D-1309 - Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant	Next

Bound With Nasa Tn D-1301-10

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