Supersonic expansion flow of an ionized gas

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

David S. Dolling

1995

A numerical method for solving the three-dimensional parabolized Navier-Stokes equations

Domenic D'Ambrosio

1995

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

Kamlesh Kapoor

1994

An investigation of bleed configurations and their effect on shock wave/boundary layer interactions

A. Hamed

1995

Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

Royce D. Moore

1987

Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

Donald R. Boldman

1987

Numerical calculations of shock-wave/boundary-layer flow interactions

P. G. Huang

1994

An investigation of the flow characteristics in the blade endwall corner region

Birinchi Hazarika

1987