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EXPERIMENTAL PERFORMANCE EVALUATION OF A 4.59-INCH RADIAL-INFLOW TURBINE WITH AND WITHOUT SPLITTER BLADES

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BookPublisher: Nasa, Washington, D.C. 1970Description: 19.DDC classification: NASA | TN D-7015

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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-7015 (Browse shelf)	Not for loan		TR13077

Total holds: 0

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Previous	NASA TN D-7012 A SEMIEMPIRICAL MODEL FOR BOUNDARY LAYER DIFFUSION IN FORCED CONVECTION FLOW	NASA TN D-7013 COMPUTER CODE FOR THE ANALYSIS OF MULTILAYERED FIBER COMPOSITES-USERS MANUAL	NASA TN D-7014 REINGESTION CHARACTERISTICS AND INLET FLOW DISTORTION OF V/STOL LIFT-ENGINE FIGHTER CONFIGURATIONS	NASA TN D-7015 EXPERIMENTAL PERFORMANCE EVALUATION OF A 4.59-INCH RADIAL-INFLOW TURBINE WITH AND WITHOUT SPLITTER BLADES	NASA TN D-7016 COMPARISON OF PREDICTED AND EXPERIMENTAL CAVITATION PERFORMANCE OF 84 (DEGRE) HELICAL INDUCER IN WATER AND HYDROGEN	NASA TN D-7017 HYPERVELOCITY PARTICLE ACCELERATOR EVALUATION	NASA TN D-7019 GASEOUS-HELIUM REQUIREMENTS FOR THE DISCHARGE OF LIQUID HYDROGEN FROM A 3.96-METER-(13-FT) DIAMETER SPHERICAL TANK	Next

Bound With Nasa Tn D-7010-7014,7016-7019

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