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AERODYNAMIC EVALUATION OF TWO-STAGE AXIAL-FLOW TURBINE DESIGNED FOR BRAYTON-CYCLE SPACE POWER SYSTEM

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BookPublisher: Nasa, Washington, D.C. Description: 28.DDC classification: NASA | TN D-4382

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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-4382 (Browse shelf)	Not for loan		TR15086

Total holds: 0

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Previous	NASA TN D-4379 EFFECTS OF COMPOSITION AND HEAT TREATMENT ON HIGH-TEMPERATURE STRENGTH OF ARC-MELTED TUNGSTEN-HAFNIUM-CARBON ALLOYS	NASA TN D-438 PROBLEMS INVOLVED IN AN EMERGENCY METHOD OF GUIDING A GLIDING VEHICLE FROM HIGH ALITUDES TO A HIGH KEY POSITION.	NASA TN D-4380 PERFORMANCE STUDY OF ROTATING GAS JET GENERATOR FOR STRONG TRAVELING TRANSVERSE ACOUSTIC MODES	NASA TN D-4382 AERODYNAMIC EVALUATION OF TWO-STAGE AXIAL-FLOW TURBINE DESIGNED FOR BRAYTON-CYCLE SPACE POWER SYSTEM	NASA TN D-4383 PERFORMANCE IN AIR OF 40INCH-(10.16-CM-) MEAN-DIAMETER SINGLE-STAGE AXIAL-FLOW TURBINE FOR REYNOLDS NUMBERS FROM 4900 TO 188 000	NASA TN D-4385 CORRELATION OF TRANSIENT SPECTRA WITH PERFORMANCE IN COAXIAL PLASMA GUNS	NASA TN D-4386 PARAMETRIC MASS ANALYSIS AND COMPARISON OF TWO TYPES OF REACTANT COOLING-AND-STORAGE UNITS FOR A LUNAR-BASED HYDROGEN-OXYGEN REGENERATIVE FUEL-CELL SYSTEM	Next

Bound With Nasa Tn D-4381,4383-90

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