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EXPERIMENTAL PERFORMANCE EVALUATION OF A 6.02-INCH RADIAL-INFLOW TURBINE OVER A RANGE OF REYNOLDS NUMBER

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BookPublisher: Nasa, Washington, D.C. Description: 20.DDC classification: NASA | TN D-3824

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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-3824 (Browse shelf)	Not for loan Untraceable		TR12516

Total holds: 0

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Previous	NASA TN D-3810 DECOMPOSITION CHRACTERISTICS OF A CHAR-FORMING PHENOLIC POLYMER USED FOR ABLATIVE COMPOSITES.	NASA TN D-3822 EXPERIMENTAL INVESTIGATION OF ACOUSTIC LINERS TO SUPPRESS SCREECH IN HYDROGEN-OXYGEN ROCKETS	NASA TN D-3823 PRELIMINARY ANALYSIS OF THE EFFECTIVENESS OF VARIABLE-GEOMETRY GUIDE VANES TO CONTROL ROTOR-INLET FLOW CONDITIONS	NASA TN D-3824 EXPERIMENTAL PERFORMANCE EVALUATION OF A 6.02-INCH RADIAL-INFLOW TURBINE OVER A RANGE OF REYNOLDS NUMBER	NASA TN D-3825 CRACK PROPAGATION, DELAYED FAILURE, AND RESIDUAL STATIC STRENGHT OF TITANIUM, ALUMINIUM, AND STAINLESS STEEL ALLOYS IN AQUEOUS ENVIRONMENTS	NASA TN D-3826 ECCENTRICALLY STIFFENED SHALLOW SHELLS OF DOUBLE CURVATURE	NASA TN D-3827 Aerodynamic characteristics at mach 2.03 of a series of curved-leading-edge wings employing various degrees of twist and camber	Next

Bound With Nasa Tn D-3821-23,3825-30

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