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EFFECTS OF INLET-GUIDE-VANE CONFIGURATION AND RELATIVE BLADE VELOCITY ON NOISE FROM AXIAL-FLOW COMPRESSORS

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BookPublisher: Nasa, Washington, D.C. 1969Description: 25.DDC classification: NASA | TN D-5507

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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-5507 (Browse shelf)	Not for loan Untraceable		TR13687

Total holds: 0

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Previous	NASA TN D-5503 ELECTROCHEMICAL BEHAVIOR OF THE ALUMINUM ELECTRODE IN MOLTEN SALT ELECTROLYTES	NASA TN D-5505 IONIC CONDUCTIVITY OF LANTHANUM FLUORIDE	NASA TN D-5506 EFFECTS OF THREE OUTLET-ANNULUS AREA BLOCKAGE CONFIGURATIONS ON THE PERFORMANCE OF A 20-INCH (50.8-CM) AXIAL-FLOW COMPRESSOR ROTOR	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	Next

Bound With Nasa Tn D-5500-5506

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