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EFFECTS OF SIMULATED RETROROCKETS ON THE AERODYNAMIC CHARACTERISTICS OF A BODY OF REVOLUTION AT MACH NUMBERS FROM 0.25 TO 1.90

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BookPublisher: Nasa, Washington, D.C. 1962Description: 45.DDC classification: NASA | TN D-1300

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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-1300 (Browse shelf)	Not for loan		TR13855

Total holds: 0

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Previous	NASA TN D-1298 THEORY OF HIGH-SPEED-IMPACT ATTENUATION BY GAS BAGS	NASA TN D-1299 FREE-FLIGHT MEASUREMENTS OF THE STATIC AND DYNAMIC STABILITY AND DRAG OF A 10 DEGREE BLUNDED CONE AT MACH NUMBERS 3.5 AND 8.5	NASA TN D-130 USE OF A THEORETICAL FLOW MODEL TO CORRELATE DATA FOR FILM COOLING OR HEATING AN ADIABATIC WALL BY TANGENTIAL INJECTION OF GASES OF DIFFERENT FLUID PROPERTIES	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	Next

Bound With Nasa Tn D-1291-1299

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