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BLADE-ELEMENT PERFORMANCE OF 0.7 HUB-TIP RADIUS RATIO AXIAL-FLOW-PUMP ROTOR WITH TIP DIFFUSION FACTOR OF 0.43. :

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BookPublisher: NASA, WASHINGTON, D.C. 1964Description: ,20.Subject(s): FUROPYRONE | FUROPYRANDDC classification: NASA TN D-2481

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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-2481 (Browse shelf)	Not for loan		83686

Total holds: 0

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Previous	NASA TN D-24 - Calculation of supersonic flow past bodies supporting shock waves shaped like elleptic cones	NASA TN D-2433 - DIGITAL FLIGHT CONTROL RESEARCH	NASA TN D-2481 INFULENCE OF RING STIFFENERS ON INSTABILITY OF ORTHOTROPIC CYLINDERS IN AXIAL COMPRESSION.	NASA TN D-2481 BLADE-ELEMENT PERFORMANCE OF 0.7 HUB-TIP RADIUS RATIO AXIAL-FLOW-PUMP ROTOR WITH TIP DIFFUSION FACTOR OF 0.43.	NASA TN D-2482 AN INVESTIGATION OF THE DYNAMIC STABILITY AND CONTROL CHRACTERISTICS FOR A TRANSPORT CRUSISING AT A MACH NUMBER OF 3.	NASA TN D-2483 SEMICLASSICAL CALCULATION OF THE DIFFERENTIAL SCATTERING CROSS SECTION WITH CHARGE EXCHANGE	NASA TN D-2484 A MODERN TRANSISTORIZED INSTRUMENTATIONS SYSTEM FOR ACOUSTICAL DATA ACQUISITION.	Next

Bpound with NASA TN D-2481-2490.

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