Supersonic Inlets

51 books
A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport applicationKamlesh Kapoor

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

Kamlesh Kapoor

1994No page data
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inletsCharles J. Trefny
⏱ 1h 0m

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets

Charles J. Trefny

198660 pp.
Analysis of inlet-compressor acoustic interactions using coupled CFD codesUnknown Author

Analysis of inlet-compressor acoustic interactions using coupled CFD codes

Unknown Author

1998No page data
Joint US/Russia TU-144 engine ground testsUnknown Author

Joint US/Russia TU-144 engine ground tests

Unknown Author

1997No page data
Comparison of the aeroacoustics of two small-scale supersonic inletsWing Ng

Comparison of the aeroacoustics of two small-scale supersonic inlets

Wing Ng

1996No page data
Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4Scott D. Holland
⏱ 2h 20m

Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4

Scott D. Holland

1993140 pp.
Investigations in the fluid dynamics of scramjet inletsRyerson Polytechnical Institute. Dept. of Mechanical Engineering

Investigations in the fluid dynamics of scramjet inlets

Ryerson Polytechnical Institute. Dept. of Mechanical Engineering

1992No page data
Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flowsZ. C. Shi
⏱ 39m

Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows

Z. C. Shi

198639 pp.
Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computationsMiklos Sajben

Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations

Miklos Sajben

1998No page data
Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flowsJohn W. Slater

Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows

John W. Slater

2002No page data
Numerical calculation of scramjet inlet flowTomiko Ishiguro
⏱ 29m

Numerical calculation of scramjet inlet flow

Tomiko Ishiguro

199229 pp.
The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular ductMilo D. Dahl

The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct

Milo D. Dahl

1996No page data
Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental dataD. R. Reddy
⏱ 13m

Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data

D. R. Reddy

199013 pp.
A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inletsHarry E. Schulte
⏱ 47m

A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets

Harry E. Schulte

197447 pp.
Internal performance of a variable ramp mixed compression intake at Mach 3.05S. A. Fisher
⏱ 10m

Internal performance of a variable ramp mixed compression intake at Mach 3.05

S. A. Fisher

198510 pp.
On hammershock propagation in a supersonic flow fieldA. Robert Porro

On hammershock propagation in a supersonic flow field

A. Robert Porro

2002No page data
Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inletMasashi Mizukami

Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

Masashi Mizukami

1995No page data
Inlet flowfield investigationUnknown Author

Inlet flowfield investigation

Unknown Author

1984No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott Douglas Holland

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott Douglas Holland

1994No page data
Analysis of inlet-compressor acoustic interactions using coupled CFD codesA. Suresh

Analysis of inlet-compressor acoustic interactions using coupled CFD codes

A. Suresh

1998No page data
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