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STATIC AERODYNAMIC CHARACTERISTICS OF SHORT BLUNT CONES WITH VARIOUS NOSE AND BASE CONE ANGLES AT MACH NUMBERS FROM 0.6 TO 5.5 AND ANGLES OF ATTACK TO 180

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BookPublisher: Nasa, Washington, D.C. 1962Description: 35.DDC classification: NASA | TN D-1327

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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-1327 (Browse shelf)	Not for loan		TR1257

Total holds: 0

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Previous	NASA TN D-1324 ELECTRON DIFFUSION IN A TURBULENT PLASMA	NASA TN D-1325 RELATIONS BETWEEN MICROSTRUCTURE AND CREEP-RUPTURE PROPERTIES OF NICKEL -BASE ALLOYS AS REVEALED BY OVERTEMPERATURE EXPOSURES	NASA TN D-1326 MOTIONS OF A SHORT 10 BLUNITED CONE ENTERING A MARTIAN ATMOSPHERE AT ARBITRARY ANGLES OF ATTACK AND ARBITRARY PITCHING RATES	NASA TN D-1327 STATIC AERODYNAMIC CHARACTERISTICS OF SHORT BLUNT CONES WITH VARIOUS NOSE AND BASE CONE ANGLES AT MACH NUMBERS FROM 0.6 TO 5.5 AND ANGLES OF ATTACK TO 180	NASA TN D-1328 A FLIGHT DETERMINATION OF THE ATTITUDE CONTROL POWER AND DAMPING REQUIREMENTS FOR A VISUAL HOVERING TASK IN THE VARIABLE STABILITY AND CONTROL X-14A RESEARCH VEHICLE	NASA TN D-1329 INITIAL WEIGHT LOSS OF PLASTICS IN A VACUUM AT TEMPERATURES FROM 80 (DEGRE) TO 500(DEGRE) F	NASA TN D-133 MEASUREMENTS OF HEAT TRANSFER AND FRICTION COEFFICIENTS FOR HELIUM FLOWING IN A TUBE AT SURFACE TEMERATURES UP TO 5900 DEGREE R.	Next

Bound With Nasa Tn D-1321-1326,1328-1330

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