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PREDICTION OF LOCAL AND INTEGRATED HEAT TRANSFER IN NOZZLES USING AN INTEGRAL TURBULENT BOUNDARY LAYER METHOD

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BookSeries: NASA Technical Note. Publisher: NASA, Washington, D.C. 1972Description: 28p.Subject(s): Aerospace

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	(Browse shelf)	NASA TN D-6595	Not for loan		TR9349

Total holds: 0

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Previous	MIXING OF SUPERSONIC JETS INCLUDING THE EFFECTS OF TRANSVERSE PRESSURE GRADIENT USING DIFFERENCE METHODS	FIELD EVAPORATION ION SOURCE WITH POSSIBLE APPLICATION TO ELECTROSTATIC PROPULSION	HEAT TRANSFER AND BOUNDARY LAYER IN CONICAL NOZZLES	PREDICTION OF LOCAL AND INTEGRATED HEAT TRANSFER IN NOZZLES USING AN INTEGRAL TURBULENT BOUNDARY LAYER METHOD	GUIDE TO USING METEOROID-ENVIRONMENT MODELS FOR EXPERIMENT AND SPACECRAFT DESIGN APPLICATION	STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF CLOSE-COUPLED WING-CANARD CONFIGURATIONS AT MACH NUMBERS FROM 1.60 TO 2.86	MONTE CARLO ERROR ANALYSIS PROGRAM FOR NEAR-MARS, FINITE-BURN, ORBITAL TRANSFER MANEUVERS	Next

Technical Reports D-6590-96
Bound Vol. No.101254; contents: TR9345-53

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