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Performence of a trasonic compressor rotor with an aspect ratio of 6.5 [NASA TN D-7762]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. NASA 1974Description: 66p.Subject(s): Propulsion system

Contents:

Technical Note D-7762

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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-7662 (Browse shelf)	Not for loan		TR-007476

Total holds: 0

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Previous	NASA TN D-749 EXPERIMENTAL EVALUATION OF THE DECELERATION OF ALUMINUM CYLINDERS ROTATING IN A MAGNETIC FIELDS AND COMMENTS ON MANGNETIC DAMPING OF A FLYWHEEL CONTROL.	NASA TN D-750 LOCAL BUCKLING OF LONGITTUDINALLY STIFFENED CURVED PLATES.	NASA TN D-7661 Effect of strain hardening on friction behavior of iron lubricated with benzyl structures [NASA TN D-7661]	NASA TN D-7662 Performence of a trasonic compressor rotor with an aspect ratio of 6.5 [NASA TN D-7762]	NASA TN D-7664 Experimental investigation of the landing dynamics of three-legged spacecraft models [NASA TN D-7664]	NASA TN D-7665 Crack-growth behavior in thick welded plates of Inconel 718 at room and cryogenic temperatures [NASA TN D-7665]	NASA TN D-7666 Landing rates for mixed slot and ctol traffic [NASA TN D-7666]	Next

Technical Note D-7762

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