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USE OF ENERGY THICKNESS IN PREDICTION OF THROAT HEAT TRANSFER IN ROCKET NOZZLES

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BookPublisher: Nasa, Washington, D.C. 1969Description: 29.DDC classification: NASA | TN D-5356 -

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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-5356 - (Browse shelf)	Not for loan		TR8279

Total holds: 0

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Previous	NASA TN D-5353 - SOLAR ABSORPTANCES AND SPECTRAL REFLECTANCES OF 12 METALS FOR TEMPERATURES RANGING FROM 300 TO 500 K	NASA TN D-5354 - TENSILE AND CYCLIC FATIGUE PROPERTIES OF GRAPHITE FILAMENT-WOUND PRESSURE VESSELS AT AMBIENT AND CRYOGENIC TEMPERATURES	NASA TN D-5355 - DYNAMIC STRAIN AGING IN CARBIDE STRENGTHENED MOLYBDENUM ALLOYS	NASA TN D-5356 - USE OF ENERGY THICKNESS IN PREDICTION OF THROAT HEAT TRANSFER IN ROCKET NOZZLES	NASA TN D-5357 - OPTICAL SIMULATION OF A RADIO-ASTRONOMY INTERFEROMETER EXPERIMENT	NASA TN D-5358 - FIXED-BASE SIMULATOR PILOT RATING SURVEYS FOR PREDICTING LATERAL-DIRECTIONAL HANDLING QUALITIES AND PILOT RATING VARIABILITY	NASA TN D-5359 - FLIGHT MEASUREMENTS OF CANARD LOADS, CANARD BUFFETING, AND ELEVON AND WING-TIP HINGE MOMENTS ON THE XB-70 AIRCRAFT INCLUDING COMPARISONS WITH PREDICTIONS	Next

Bound With Nasa Tn D-5341-60

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