Supersonic expansion flow of an ionized gas

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

David S. Dolling

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

A. Hamed

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

Kamlesh Kapoor

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

Domenic D'Ambrosio

Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen

Reinhard Niehuis

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

P. G. Huang

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

Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel

Thomas F. Gelder

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