Effect of pressurant inlet configuration on liquid outflow in weightlessness
Pressurant inlet configuration effect on liquid outflow from cylinder in weightlessness
Berenyi, S. G.↗
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Starting criterion for hypersonic inlets
Starting criterion for hypersonic inlets with large turbulent boundary layers, considering total pressure recovery from all shock and viscous losses
Goldberg, T. J.↗
Flight performance of auxiliary inlet ejector and plug nozzle at transonic speeds
Auxiliary inlet ejector and plug nozzle flight performance, describing design variation effects for high supersonic speeds
Burley, R. R.↗
Increasing the stable operating range of a Mach 2.5 inlet
Stable operating range of supersonic mixed compression inlet increase by air flow removal via throat bleed system
Mitchell, G. A.↗
A study of the relative merits of three axisymmetric inlets for a hypersonic cruise mission
Turboramjet powered hypersonic aircraft axisymmetric inlet systems using forward translating cowl and centerbody for various air flow characteristics
Bencze, D. P.↗
The effect of inlet temperature distortion on the performance of a turbo-fan engine compressor system
Turbofan engine compressor system performance dependence on circumferential extent, magnitude and rate of change of inlet temperature in altitude test facility
Antl, R. J.↗
An approximate method for predicting annulus inlet turbulent flow development characteristics
Newtonian fluid turbulent flow development characteristics in inlet region of smooth concentric annulus from momentum integral equations
Bathie, W. W.↗
A two-dimensional mixed-compression inlet system designed to self-restart at a Mach number of 3.5
M 3.5 two dimensional mixed compression inlet system with self restart using flexible variable ramp system
Anderson, W. E.↗
Servosystem design of a high-response slotted- plate overboard bypass valve for a supersonic inlet
Servosystem design of high-response multislotted bypass valving system for supersonic inlets
Neiner, G. H.↗
Hydrologic studies in northern Cook Inlet, Alaska using color photography and thermal imagery
Infrared and color photography for water inlet survey in Alaska
Barnwell, W. W.↗
Dynamic distortion at the exit of a subsonic diffuser of a mixed compression inlet
Measuring distortion characteristics at engine face station of axisymmetric inlet
Kostin, L. C.↗
Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
Wind tunnel tests of mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
Smeltzer, D. B.↗
Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position
Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position
Cole, G. L.↗
Reingestion characteristics and inlet flow distortion of V/STOL lift-engine fighter configurations
Reingestion characteristics and inlet flow distortion of V/STOL fighter powered by J-85 engine
Barrack, J. P.↗
Numerical study of control of dynamic properties of a supersonic inlet using bypass bleed
Numerical study on controlling dynamic properties of supersonic inlet using bypass bleed
Matthews, C. W.↗
Inlet flow distortion testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Task 2 stage data and performance report
Inlet flow distortion testing of high Mach number transonic fan stages - Vol. 1
Doyle, V. L.↗
Inlet flow distortion testing. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Task 2 stage data and performance report
Tabular data derived from inlet flow distortion tests of high Mach number transonic fan stages - Vol. 2
Doyle, V. L.↗
Study and development of turbofan nacelle modifications to minimize fan-compressor noise radiation. Volume 5 - Sonic inlet development Contractor report, 1 May 1967 - 1 Nov. 1969
Static tests to determine effects of throat inlet concepts on forward-radiated fan noise of 707-320B/C airplanes
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