Sonic-throat inlets
Noise reduction test results for turbofan cowl inlet configuration of transport aircraft
Higgins, C. C.↗
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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.↗
Design of supersonic inlets by a computer program incorporating the method of characteristics
FORTRAN computer program for designing supersonic inlets by characteristic theory
Anderson, B. H.↗
Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet conditions
Butze, H. F.↗
Design and performance of flueric shock position sensor for a mixed-compression supersonic inlet
Design and performance of flueric shock position sensor for mixed compression supersonic inlets
Griffin, W. S.↗
Theoretical analysis of flow in VTOL lift fan inlets without crossflow
Theoretical analysis of axisymmetric flow in VTOL lift fan inlets without crossflow
Lieblein, S.↗
Performance characteristics from Mach 2.58 to 1.98 of an axisymmetric mixed-compression inlet system with 60-percent internal contraction
Performance test from Mach 2.58 to 1.98 of axisymmetric mixed-compression inlet system with 60 percent internal contraction
Cubbison, R. W.↗
Single stage experimental evaluation of variable geometry guide vanes and stator blading. Part 5 - Overall performance for variable camber guide vane and stator B with radial and circumferential inlet flow distortion
Inlet flow distortion effects on single stage variable geometry guide vanes and stators
Clark, C. E.↗
Characteristics study of a bicone mixed- compression inlet for Mach 1.80 to 2.50
Characteristics study of bicone mixed compression inlet for Mach 1.80 to 2.50
Anderson, B. H.↗
Steady-state interactions from Mach 1.98 to 2.58 between a turbojet engine and an axisymmetric inlet with 60-percent internal area contraction
Steady-state interactions between turbojet engine and axisymmetric inlet with induced distortions
Choby, D. A.↗
Restart and high response terminal shock control for an axisymmetric mixed-compression inlet with 60-percent internal contraction
Restart and high response terminal shock control for axisymmetric mixed-compression inlet with internal contraction
Cole, G. L.↗
Experimental data for two 1400-feet per second tip speed compressor rotors operated with inlet flow distortions
Performance data for high tip speed compressor rotor operated with radial and inlet airflow distortions
Bailey, E. E.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 5 - Performance of plain casing insert configuration with distorted inlet flow
Outer case bleeding or blowing effects on casing insert of single stage axial flow compressor with distorted inlet flow
Koch, C. C.↗
Performance and stall limits of a YTF30-P-1 turbofan engine with uniform inlet flow
Performance and stall limits of YTF30-P-1 turbofan engine with uniform compressor inlet flow
Braithwaite, W. M.↗
The vortex at an inlet of an air intake
Vortex at air intake inlet investigated by direct air flow visualization techniques
Miroshnichenko, A. YA.↗