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EFFECTS OF A REDUCTION IN BLADE THICKNESS ON PERFORMANCE OF A SINGLE-STAGE 20.32-CENTIMETER MEAN-DIAMETER TURBINE.

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BookPublisher: Nasa, Washington, D.C. 1973Description: 24.DDC classification: NASA | TN D-7128

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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-7128 (Browse shelf)	Not for loan		TR12008

Total holds: 0

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Previous	NASA TN D-7125 SINGLE-THRUST-PERIOD MISSIONS TO URANUS FOR UNMANNED NUCLEAR-ELECTRIC PROPULSION SYSTEMS.	NASA TN D-7126 DETERMINATION OF THE TEMPERATURE OF GAS MIXTURES BY USING LASER RAMAN SCATTERING.	NASA TN D-7127 LOCAL HEAT-TRANSFER CHARACTERISTICS OF A ROW OF CIRCULAR AIR JETS IMPINGING ON A CONCAVE SEMICYLINDRICAL SURFACE.	NASA TN D-7128 EFFECTS OF A REDUCTION IN BLADE THICKNESS ON PERFORMANCE OF A SINGLE-STAGE 20.32-CENTIMETER MEAN-DIAMETER TURBINE.	NASA TN D-7129 FIRST-ORDER OPTICAL ANALYSIS OF A QUASI-MICROSCOPE FOR PLANETARY LANDERS.	NASA TN D-713 A PRELIMINARY STUDY OF THE USE OF FINITE-THRUST ENGINES FOR ABORT DURING LAUNCH OF SPACE VEHICLES	NASA TN D-7133 EVALUATION OF MAGNESIUM-LAUMINUM EUTECTIC TO IMPROVE COMBUSTION EFFICIENCY IN LOW BURNING-RATE PROPELLANTS.	Next

Bound With Nasa Tn D-7120-27, 7129

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