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EFFECT OF COMPONENT DIFFERENTIAL HARDNESSES ON ROLLING-CONTACT FATIGUE AND LOAD CAPACITY

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BookPublisher: Nasa, Washington, D.C. 1965Description: 21.DDC classification: NASA | TN D-2640 -

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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-2640 - (Browse shelf)	Not for loan		TR9749

Total holds: 0

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Previous	NASA TN D-2637 - EVALUATION OF 40-MILLIMETER-BORE BALL BEARINGS OPERATING IN LIQUID OXYGEN AT DN VALUES TO 1.2 MILLION	NASA TN D-2638 - MAGNETIC SUSCEPTIBILITIES OF COMPOSITIONS IN TANTALUM-TANTALUM CARBIDE SYSTEM	NASA TN D-2639 - EXPERIMENTAL INVESTIGATION OF A 3.0-INCH-MEAN-DIAMETER FULL-ADMISSION THREE-STAGE TURBINE SUITABLE FOR SMALL AUXILIARY POWER UNITS	NASA TN D-2640 - EFFECT OF COMPONENT DIFFERENTIAL HARDNESSES ON ROLLING-CONTACT FATIGUE AND LOAD CAPACITY	NASA TN D-2711 Effects of impurities on radiation damage of silicon solar cells [NASA TN D-2711]	NASA TN D-2712 Analysis of turbopump feed systems for hydrogen-nuclear rockets [NASA TN D-2712]	NASA TN D-2713 Aerodynamic damping and buffet response of an aeroelastic model of the saturn I block II launch vehicle [NASA TN D 2713]	Next

Bound With Nasa Tn D-2631-40

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