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DESIGN AND OVERALL PERFORMANCE OF AN AXIAL FLOW-PUMP ROTOR WITH A BLADE TIP DIFFUSION FACTOR OF 0.43

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BookPublisher: Nasa, Washington, D.C. 1964Description: 27.DDC classification: NASA | TN D-2295 -

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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-2295 - (Browse shelf)	Not for loan		TR8985

Total holds: 0

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Previous	NASA TN D-2292 - EXPERIMENTAL INVESTIGATION OF THE DYNAMIC STABILITY OF A TOWED PARAWING GLIDER AIR CARGO DELIVERY SYSTEM	NASA TN D-2293 - EXPERIMENTAL FLUTTER RESULTS FOR CORRUGATION-STIFFENED PANELS AT A MACH NUMBERS OF 3	NASA TN D-2294 - A CORRELATION OF FILM-BOILING HEAT-TRANSFER COEFFICIENTS OBTAINED WITH HYDROGEN, NITROGEN, AND FREON 113 INFORCED FLOW	NASA TN D-2295 - DESIGN AND OVERALL PERFORMANCE OF AN AXIAL FLOW-PUMP ROTOR WITH A BLADE TIP DIFFUSION FACTOR OF 0.43	NASA TN D-2296 - MONTE CARLO COMPUTATION OF THE STATISTICS OF THE MIDCOURSE VELOCITY CORRECTIONS FOR A LUNAR MISSION	NASA TN D-2297 - COMPARISONS OF SOME WING FLUTTER CHARACTERISTICS OBTAINED BY MODIFIED STRIP ANALYSIS, SUBSONIC KERNEL FUNCTION, AND EXPERIMENT	NASA TN D-2298 - FORCES ACTING ON BUBBLES IN NUCLEATE BOILING UNDER NORMAL AND REDUCED GRAVITY CONDITIONS	Next

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