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EFFECT OF COMPONENT DIFFERENTIAL HARDNESS ON RESIDUAL STRESS AND ROLLING-CONTACT FATIGUE

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BookPublisher: Nasa, Washington, D.C. 1965Description: 14.DDC classification: NASA | TN D-2664

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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-2664 (Browse shelf)	Not for loan		TR16162

Total holds: 0

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Previous	NASA TN D-2660 THEORY AND OPERATION OF VARIABLE EXPOSURE PHOTOGRAPHIC PYROMETER OVER THE TEMPERATURE RANGE 1800 DEGREE TO 3600 DEGREE F (1255 DEGREE TO 2255 DEGREE K )	NASA TN D-2662 INCIPIENT CAVITATION OF FREON-114 IN A TUNNEL VENTURI	NASA TN D-2663 EVALUATION OF FIVE BEARING-SEPARATOR MATERIALS AND POLYPHENYL ETHER LUBRICANTS AND POLYPHENYL ETHER LUBRICANTS FOR USE IN SPACE POWER GENERATION SYSTEMS	NASA TN D-2664 EFFECT OF COMPONENT DIFFERENTIAL HARDNESS ON RESIDUAL STRESS AND ROLLING-CONTACT FATIGUE	NASA TN D-2665 REMOTE MANIPULATION WITH TRANSMISSION DELAY	NASA TN D-2666 FREE VIBRATIONS OF CONICAL SHELLS	NASA TN D-2667 A STANDARD TELEMETRY PACKAGE FOR NIKE-CAJUN AND NIKE-APACHE SOUNDING ROCKETS	Next

Bound With Nasa Tn D-2661-63,2665-70

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