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supersonic diffusers

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

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

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

By Kamlesh Kapoor

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

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

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

By Masashi Mizukami

View 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet By M. Mizukami

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By M. Mizukami

View Factors affecting the performance of supersonic diffusers By A. M. Patterson

Factors affecting the performance of supersonic diffusers

Factors affecting the performance of supersonic diffusers

By A. M. Patterson

View 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet By Masashi Mizukami

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By Masashi Mizukami

View Supersonic inlets By Ione D. V. Faro

Supersonic inlets

Supersonic inlets

By Ione D. V. Faro

View Further tests with a variable ramp intake having a design Mach number of 2.2 By M. C. Neale

Further tests with a variable ramp intake having a design Mach number of 2.2

Further tests with a variable ramp intake having a design Mach number of 2.2

By M. C. Neale

View Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 By John M. Smith

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

By John M. Smith

View Supersonic diffusors for large pressure recovery By Kenneth C. Livingston

Supersonic diffusors for large pressure recovery

Supersonic diffusors for large pressure recovery

By Kenneth C. Livingston

View Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 By John M Smith

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

By John M Smith

View Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 By John M. Smith

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

By John M. Smith