Experimental results of a transpiration-cooled turbine operated in an engine for 150 hours at 2500 F turbine inlet temperature.
Testing of transpiration air cooled turbine, discussing blade fabrication
AIR COOLING↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Leading edge bluntness effects and their importance in hypersonic inlet design.
Shock and boundary layers about blunted two- dimensional slender bodies in hypersonic flow
SLENDER BODY↗
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. 4 - Performance of first stage with modified inlet feedpipe-manifold assembly
Aerodynamic performance of scale model oxygen pump-drive turbine for M-1 rocket engine
Kline, J. F.↗
Priming an air inlet in unsteady flow at Mach 7
Priming air intakes in unsteady hypersonic flow
Bourgeois, J. P.↗
Sound measurements on a full-scale jet-engine inlet-noise-suppressor cowling
Acoustic measurements on jet engine intake system noise reduction suppressor cowlings
Acker, L. W.↗
Turbojet-engine noise studies to evaluate effects of inlet-guide-vane-rotor spacing
Turbojet engine noise reduction by increasing intake system guide vane-rotor blade spacing
Copeland, W. L.↗
Tests of a single tube-in-shell water-boiling heat exchanger with a helical-wire insert and several inlet flow-stabilizing devices
Single tube-in-shell water-boiling heat exchanger performance with helical wire insert and flow stabilizing devices
Sekas, N. J.↗
An experimental investigation of the air- flow stability of a scoop-type normal-shock inlet
Explore the source record for details and available documents.
Lazzeroni, F. A.↗
Ground-runup tests of acoustically treated inlets and fan ducts
Ground performance tests on noise intensity of turbofan engine ducts modified by acoustic linings
Marsh, A. H.↗
Influence of high-turbine inlet temperature engines in a methane-fueled SST when takeoff jet noise limits are considered
Afterburning turbojet, nonafterburning turbojet, and duct burning turbofan designs for supersonic transports with and without takeoff noise constraints
Koenig, R. W.↗
Experimental investigation of dynamic distortion in a Mach 2.50 inlet with 60 percent internal contraction and its effect on turbojet stall margin
Dynamic distortion of supersonic wind tunnel for turbojet engines
Calogeras, J. E.↗
Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70
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Bond, A. C.↗
Technique for inducing controlled steady-state and dynamic inlet pressure disturbances for jet engine tests
Secondary air injection achieving momentum interchanges to induce controlled steady state dynamic pressure disturbances for jet engine tests
Biesiadny, T. J.↗
Experimental cavitation and flashing of potassium flowing adiabatically through a Venturi sized as a boiler inlet
Cavitation and flashing of potassium flowing adiabatically through Venturi
Fenn, D. B.↗
Design of disk-gap-band and modified ringsail parachutes and development of ballute apex inlet for supersonic application
Design of parachutes and ballutes for decelerating atmospheric entries at supersonic velocities
Faurote, G. L.↗
Telescoping-spike supersonic inlet for aircraft engines Patent
Telescoping-spike supersonic nozzle for turbojet or ramjet engines
Connors, J. F.↗
Racemization of amino acids in sediments from Saanich Inlet, British Columbia
Amino acid racemization as enantiomers in core sediment samples
Brown, F. S.↗
Aerodynamic characteristics of a large-scale model with a lift fan mounted in a 5 per cent thick triangular wing, including the effects of BLC on the lift fan inlet
Aerodynamic characteristics of large-scale model with lift fan mounted in 5 percent thick triangular wing
Hall, L. P.↗