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EFFECT OF AUTOCLAVE HEAT TREATMENTS ON THE MECHANICAL PROPERTIES OF THE PREALLOYED POWDER COBALT-BASE ALLOY HS-31

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BookPublisher: Nasa, Washington, D.C. 1973Description: 22.DDC classification: NASA | TN D-7117

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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-7117 (Browse shelf)	Not for loan		TR12403

Total holds: 0

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Previous	NASA TN D-7114 EXTRACTION OF LONGITUDINAL AERODYNAMIC COEFFICIENTS FROM FORWARD-FLIGHT CONDITIONS OF A TILT WING V/STOL AIRPLANE	NASA TN D-7115 MINIMUM WEIGHT DESIGN OF STRUCTURES VIA OPTIMALITY CRITERIA	NASA TN D-7116 POSITION DETERMINATION ACCURACY FROM THE MICROWAVE LANDING SYSTEM	NASA TN D-7117 EFFECT OF AUTOCLAVE HEAT TREATMENTS ON THE MECHANICAL PROPERTIES OF THE PREALLOYED POWDER COBALT-BASE ALLOY HS-31	NASA TN D-7118 EMISSION OF SOUND FROM TURBULENCE CONVECTED BY A PARALLEL FLOW IN THE PRESENCE OF SOLID BOUNDARIES	NASA TN D-7119 ELASTOSTATIC STRESS ANALYSIS OF ORTHOTROPIC RECTANGULAR CENTER-CRACKED PLATES	NASA TN D-712 INVESTIGATION AT TRANSONIC SPEEDS OF THE LOADING OVER A 45 DEGREE SWEPTBACK WING HAVING AN ASPECT RATIO OF 3, A TAPER RATIO OF 0.2, AND NACA 65A004 AIRFOIL SECTIONS	Next

Bound With Nasa Tn D-7110-16, 7118-19.

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