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RESEARCH TURBINE FOR HIGH-TEMPERATURE CORE ENGINE APPLICATION.

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BookPublisher: Nasa, Washington, D.C. 1974Description: 27.DDC classification: NASA | TN D-7639

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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-7639 (Browse shelf)	Not for loan		TR12548

Total holds: 0

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Previous	NASA TN D-7636 EFFECT OF GEOMETRICAL AND FLOW PARAMETERS ON HIGH-EFFECTIVENESS REGION OF FILM COOLING.	NASA TN D-7637 APPLICATION OF BOUNDARY INTEGRAL METHOD TO ELASTROPLASTIC ANALYSIS OF V-NOTCHED BEAMS.	NASA TN D-7638 PRESSURANT REQUIREMENTS FOR DISCHARGE OF LIQUID METHANE FORM A 1.52-METER-(5-FT-) DIAMETER SPHERICAL TANK UNDER BOTH STATIC AND SLOSH CONIDTIONS.	NASA TN D-7639 RESEARCH TURBINE FOR HIGH-TEMPERATURE CORE ENGINE APPLICATION.	NASA TN D-764 EXAMINATION OF PRESSURE OSCILLATIONS INDUCED BY CHANGES IN THE BURNING RATE OF FLAMES	NASA TN D-7640 A MARKOVIAN MODEL FOR ASSESSMENT OF PERSONNEL HIRING PLANS.	NASA TN D-7642 NONLINEAR MODELS FOR ESTIMATING GSFC TRAVEL REQUIREMENTS.	Next

Bound With Nasa Tn D-7631-38,7640.

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