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EXPERIMENTAL EVALUATION OF A TF30-P-3 TURBOFAN ENGINE IN AN ALTITUDE FACILITY : AFTERBURNER PERFORMANCE AND ENGINE-AFTERBURNER OPERATING LIMITS

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BookPublisher: Nasa, Washington, D.C. 1972Description: 34.DDC classification: NASA | TN D-6839

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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-6839 (Browse shelf)	Not for loan		TR14267

Total holds: 0

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Previous	NASA TN D-6836 NEW METHODS FOR PREPARING N,N-DIALKYLTRIFLUOROACETAMIDS	NASA TN D-6837 INFLUENCE OF POROUS-WALL THERMAL EFFECTIVENESS ON TURBULENT-BOUNDARY-LAYER HEAT TRANSFER	NASA TN D-6838 THE 1200(DEGRE) C CYCLIC OXIDATION BEHAVIOR OF TWO NICKEL-ALUMINUM ALLOYS (NI3A1 AND NIA1) WITH ADDITIONS OF CHROMIUM,SILICON, AND TITANIUM	NASA TN D-6839 EXPERIMENTAL EVALUATION OF A TF30-P-3 TURBOFAN ENGINE IN AN ALTITUDE FACILITY	NASA TN D-684 IGNITION OF HYDROGEN-OXYGEN ROCKET COMBUSTOR WITH CHLORINE TRIFLUORIDE AND TRIETHYLALUMINUM	NASA TN D-6841 EFFECT OF EDDY DIFFUSIVITY ON WIND-DRIVEN CURRENTS IN A TWO-LAYER STRATIFIED LAKE.	NASA TN D-6842 CYCLIC OXIDATION OF COBALT-CHROMIUM-ALUMINUM-YTTRIUM AND ALUMINIDE COATINGS ON IN-100 AND VIA ALLOYS IN HIGH-VELOCITY GASES.	Next

Bound With Nasa Tn D-6830-6838

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