Noise reduction by means of inlet-guide-vane choking in an axial-flow compressor
Inlet guide vane choking noise reduction in axial flow compressors
Chestnutt, D.↗
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Experimental evaluation of outer casing blowing or bleeding of single stage axial flow compressor. Part 2 - Performance of plain casing insert configuration with undistorted inlet flow and boundary layer trip
Outer casing blowing and bleeding and undistorted inlet flow for improved performance of high aspect ratio transonic rotor
Koch, C. C.↗
Experimental investigation of the dynamic response of a supersonic inlet to external and internal disturbances
Dynamic response of subsonic inlet to external and internal disturbances
Wasserbauer, J. F.↗
Variable geometry requirements in inlets and exhaust nozzles for high Mach number applications
Variable geometry requirements in exhaust nozzles and inlets for high Mach number applications
Beheim, M. A.↗
Experimental and analytical investigation of the dynamic response of a supersonic mixed-compression inlet
Experimental and analytical investigation of dynamic response of supersonic mixed-compression inlet
Wasserbauer, J. F.↗
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.↗
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.↗