High performance bypass control for mixed-compression inlets
Shock and restart control systems with bypass doors and pressure transducers for mixed compression inlets
Cole, G. L.↗
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Results for “Inlet”
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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Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraft
Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraft
Jones, J. R.↗
Investigation of vitiated inlet-air effects on turbojet engine performance
Inlet air pollution effects on turbojet engine performance
Snyder, D. R.↗
Effect of uncooled inlet length and nozzle convergence angle on the turbulent boundary layer and heat transfer in conical nozzles operating with air.
Turbulent boundary layer and heat transfer coefficients for air in conical nozzles, noting uncooled inlet length and convergence angle effects
Boldman, D. R.↗
Effect of inlet boundary-layer thickness and structure on heat transfer in a supersonic nozzle.
Inlet boundary layer thickness and structure effects on heat transfer in supersonic nozzle
Back, L. H.↗
Reingestion characteristics and inlet flow distortion of V/STOL lift engine fighter configurations.
Exhaust gas reingestion and inlet flow distortion in V/STOL lift engines, discussing static and wind tunnel testing using fighter configuration models
Barrack, J. P.↗
Study of a family of supersonic inlet systems.
Large scale axisymmetric inlet systems performance capabilities, reviewing theoretical and experimental programs
Cubbison, R. W.↗
Experimental and analytical investigation of the dynamic response of a supersonic mixed- compression inlet.
Dynamic response of shock position resulting from internal disturbances for supersonic mixed compression inlet
Wasserbauer, J. F.↗
High performance bypass control for mixed- compression inlets.
Bypass control for mixed compression inlets, discussing normal shock and restart control systems utilizing bypass doors and pressure transducers
Cole, G. L.↗
Variable geometry requirements in inlets and exhaust nozzles for high Mach number applications.
Variable geometry supersonic aircraft design, discussing inlet and exhaust nozzles problems and wind tunnel tests
Beheim, M. A.↗
Water flow and cavitation in converging- diverging boiler-inlet nozzle
Water flow and cavitation in convergent-divergent boiler inlet nozzles
Sekas, N. J.↗
Effect of porous bleed in a high performance axisymmetric, mixed compression inlet at Mach 2.50
Effects of boundary layer bleed rate and location on performance of axisymmetric inlet designed for Mach 2.5
Cubbison, R. W.↗
Performance of inlet sound suppressors
Theoretical model and acoustic attenuation measurements for inlet noise suppressors
Feiler, C. E.↗
Sonic-throat inlets
Noise reduction test results for turbofan cowl inlet configuration of transport aircraft
Higgins, C. C.↗
Treated inlets
Design of lined ring inlet for reduced noise sound pressure levels of Boeing 707 aircraft engine
Drakeley, G. T.↗
Preliminary investigation of distortion dynamics in a Mach 3 mixed compression inlet
Wind tunnel tests of distortion dynamics in Mach three mixed compression inlet
Coltrin, R. E.↗
Effect of bleed-system back pressure and porous area on the performance of an axisymmetric mixed-compression inlet at Mach 2.50
Performance tests of wind tunnel model inlet for bleed system back pressure and porous area effect of axisymmetric compression
Cubbison, R. W.↗
A mathematical analysis of supersonic inlet dynamics
Approximate mathematical analysis of supersonic inlet dynamics
Willoh, R. G.↗