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ANALYTICAL INVESTIGATION OF PERFORMANCE OF TWO-STAGE TURBINE OVER A RANGE OF RATIOS OF SPECIFIC HEATS FROM 1.2 TO 1 AND 2/3

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BookPublisher: Nasa,Washington, D.C. 1962Description: 45.DDC classification: NASA | TN D-1288 -

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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-1288 - (Browse shelf)	Not for loan		TR9730

Total holds: 0

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Previous	NASA TN D-1285 - EMPIRICAL CORRELATION OF CRITICAL BOILING HEAT FLUX IN FORCED FLOW UPWARD THROUGH UNIFORMLY HEATED TUBES	NASA TN D-1286 - ANALYTICAL DETERMINATION OF TEMPERATURE OSCILLATIONS IN A WALL HEATED BY ALTERNATING CURRENT	NASA TN D-1287 - EXPERIMENTAL INVESTIGATION OF WATER-ABSORBENT MATERIALS AS POSSIBLE HEAT SINKS FOR HYPERSONIC AND REENTRY VEHICLES	NASA TN D-1288 - ANALYTICAL INVESTIGATION OF PERFORMANCE OF TWO-STAGE TURBINE OVER A RANGE OF RATIOS OF SPECIFIC HEATS FROM 1.2 TO 1 AND 2/3	NASA TN D-1289 - ABSORPTION AND EMISSION CHARACTERISTICS OF DIFFUSE SPHERICAL ENCLOSURES	NASA TN D-129 COMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO	NASA TN D-1290 - ADDITION TO THE YALE TABLES FOR THE DEVELOPMENT OF THE DISTURBING FUNCTION	Next

Bound With Nasa Tn D-1281-90

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