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SUBSONIC PERFORMANCE CHARACTERISTICS OF A LARGE-SCALE 1.075-PRESSURE-RATIO TIP-TURBINE CRUISE-FAN PROPULSION SYSTEM

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BookPublisher: Nasa, Washington, D.C. 1969Description: 276.DDC classification: NASA | TN D-5314 -

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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-5314 - (Browse shelf)	Not for loan		TR9290

Total holds: 0

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Previous	NASA TN D-5310 THERMOELASTIC INSTABILITY OF OPEN-SECTION BOOMS	NASA TN D-5312 - ANALOG COMPUTER STUDY OF THE LOW-FREQUENCY FLOW DYNAMICS OF TWO NUCLEAR-ROCKET COLD-FLOW ENGINE SYSTEMS	NASA TN D-5313 - GROWTH OF 2H SILICON CARBIDE CRYSTALS	NASA TN D-5314 - SUBSONIC PERFORMANCE CHARACTERISTICS OF A LARGE-SCALE 1.075-PRESSURE-RATIO TIP-TURBINE CRUISE-FAN PROPULSION SYSTEM	NASA TN D-5315 - EXPERIMENTAL INVESTIGATION OF THE MIXING OF COMPRESSIBLE-AIR JETS IN A COAXIAL CONFIGURATION	NASA TN D-5316 - SUBSONIC AERODYNAMIC CHARACTERISTICS OF A LARGE-SCALE 1.075-PRESSURE-RATIO TIP-TURBINE CRUISE-FAN PROPULSION SYSTEM AT ANGLE OF ATTACK	NASA TN D-5318 - EFFECT OF FLUID TEMPERATURE ON THE CAVITATION PERFORMANCE OF A HIGH HUB-TIP RATIO AXIAL FLOW PUMP IN WATER TO 250(DEGREE) F (394 K)	Next

Bound With Nasa Tn D-5311-20

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