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EXPERIMENTAL RESULTS OF VARYING THE BLADE-SHROUD CLEARANCE IN A 6.02-INCH RADIAL-INFLOW TURBINE

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BookPublisher: Nasa, Washington, D.C. 1970Description: 22.DDC classification: NASA | TN D-5513

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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-5513 (Browse shelf)	Not for loan		TR15201

Total holds: 0

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Previous	NASA TN D-5507 EFFECTS OF INLET-GUIDE-VANE CONFIGURATION AND RELATIVE BLADE VELOCITY ON NOISE FROM AXIAL-FLOW COMPRESSORS	NASA TN D-5511 APPLICATION OF MODERN NETWORK THEORY TO ANALYSIS OF COMPLEX SYSTEMS	NASA TN D-5512 INVESTIGATION OF LAMINAR AND TURBULENT BOUNDARY LAYERS INTERACTING WITH EXTERNALLY GENERATED SHOCK WAVES	NASA TN D-5513 EXPERIMENTAL RESULTS OF VARYING THE BLADE-SHROUD CLEARANCE IN A 6.02-INCH RADIAL-INFLOW TURBINE	NASA TN D-5514 WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC PRESSURES ON THE APOLLO COMMAND MODULE CONFIGURATION	NASA TN D-5515 THE EFFECT OF OBJECT MOTION IN FRAUNHOFER HOLOGRAPHY WITH APPLICATION TO VELOCITY MEASUREMENTS	NASA TN D-5516 A METHOD FOR SOLVING THE NONSIMILAR LAMINAR BOUNDARY-LAYER EQUATIONS INCLUDING FOREIGN GAS INJECTION	Next

Bound With Nasa Tn D-5510-12,5514-18

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