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EFFECTS OF MODEL GEOMETRIC ACCURACY ON COMPARISON OF WIND-TUNNEL AND FLIGHT PRESSURE MEASUREMENTS ON A LAUNCH VEHICLE

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BookPublisher: Nasa, Washington, D.C. 1966Description: 26.DDC classification: NASA | TN D-3274

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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-3274 (Browse shelf)	Not for loan		TR11994

Total holds: 0

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Previous	NASA TN D-327 A TECHNIQUE FOR DETEMINING RELAXATION TIMES BY FREE- FLIGHT TESTS OF LOW- FINENESS- RATIO CONES; WITH EXPERIMENTAL RESULTS TEMERATURES UP TO 3440 DEGREE K	NASA TN D-3272 EXPERIMENTAL STUDY OF STAGNATION ENTHALPY IN THE LANGLEY HOTSHOT TUNNEL	NASA TN D-3273 AN ALGORITHM FOR SYNTHESIS OF SYNCHRONOUS SEQUENTIAL CIRCUITS	NASA TN D-3274 EFFECTS OF MODEL GEOMETRIC ACCURACY ON COMPARISON OF WIND-TUNNEL AND FLIGHT PRESSURE MEASUREMENTS ON A LAUNCH VEHICLE	NASA TN D-3275 A STUDY OF SEVERAL OXIDATION-RESISTANT COATINGS ON CB-10 TI-5 ZR ALLOY SHEET AT 2000 DEGREE F, 2400 DEGREE F, AND 2700 DEGREE F (1365 DEGREE K, AND 1755 DEGREE K)	NASA TN D-3276 EFFECT OF GEOMETRIC MODIFICATIONS ON THE MAXIMUM LIFT -DRAG RATIOS OF SLENDER WING-BODY CONFIGURATIONS AT HYPERSONIC SPEEDS	NASA TN D-3277 MASS-FLOW RATES AND TOTAL-PRESSURE RECOVERIES FOR A SEMICIRCULAR OPEN-NOSE INLET AT MACH 6	Next

Bound With Nasa Tn D-3271-73, 3275-80.

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