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Effect of exposure cycle on hot-salt stress-corrosion of a titanium alloy : National Aeronautics and Space Administration

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C Ohio Description: 18p.Subject(s): Titaniam alloyDDC classification: TR | TMX-3145

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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	TR TMX-3145 (Browse shelf)	Not for loan		TR2746

Total holds: 0

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Previous	TR TMX-3129 Experimental aerodynamic charaeter istics for bodies of elliptic cross section at angles of attack from O to 58 and much numbers from 0.6 to 2.0	TR TMX-3130 Experimental aerodynaics characteristics for a cylindrical body of vevolution with side strakes and various noses at angles of attack from O to 58 and mach numbers from 0.6 to 2.0	TR TMX-3136 Refinement in black chrome for use as a solar selectire coating	TR TMX-3145 Effect of exposure cycle on hot-salt stress-corrosion of a titanium alloy	TR TMX-3146 Spontaneous-ignition temperature limits of jet a fuel in research-combustor segment	TR TMX-3147 Tests of protective clathing for the safe handling of pressurized lamps	TR TMX-3148 Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor	Next

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