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HOT-SALT STRESS-CORROSION OF A TITANIUM ALLOY UNDER A SIMULATED TURBINE-ENGINE COMPRESSOR ENVIRONMENT

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BookPublisher: NASA, WASHINGTON, D.C. 1969Description: ,35.DDC classification: NASA | TN D-5510

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-5510 (Browse shelf)	Not for loan		101171

Total holds: 0

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Previous	NASA TN D-5441 ABSORPTION OF HYDROGEN BY PALLADIUM AND ELECTRICAL RESISTIVITY UP TO HYDROGEN-PALLADIUM ATOM RATIOS OF 0.97	NASA TN D-5451 A MINIATURE ELECTROMECHANICAL TUNNEL DIODE TRANSDUCER	NASA TN D-5491 FLIGHT EVALUATION OF TIP-TURBINE-DRIVEN FANS FOR LATERAL CONTROL IN A HOVERING VTOL AIRCRAFT	NASA TN D-5510 HOT-SALT STRESS-CORROSION OF A TITANIUM ALLOY UNDER A SIMULATED TURBINE-ENGINE COMPRESSOR ENVIRONMENT	NASA TN D-5520 CONVECTIVE HEAT-TRANSFER COEFFICIENTS FROM A SOLUTION OF THE CONDUCTION EQUUATION FOR A WALL SEPRATING TWO FLUIDS, ONE HAVING AN OSCILLATING TEMPERATURE.	NASA TN D-5530 INTERACTION OF 42-MEV ALPHA PARTICLES WITH HELIUM-3	NASA TN D-5570 PERFORMANCE OF SHORT LENGTH TURBOJET COMBUSTOR INSENSITIVE TO RADIAL DISTORTION OF INLET AIRFLOW	Next

Bound with NASA TN D-5511-5518

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