Supersonic diffusers

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

M. Mizukami and J.D. Saunders.

Supersonic inlets

by Ione D. V. Faro.

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

Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.

Factors affecting the performance of supersonic diffusers

A. M. Patterson.

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

by M. C. Neale and P. S. Lamb.

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

M. Mizukami and J.D. Saunders.

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

M. Mizukami and J.D. Saunders.

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

John M. Smith and Albert J. Juhasz

Supersonic diffusors for large pressure recovery

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

John M. Smith and Albert J. Juhasz.