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by A. Hamed
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Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
David S. Dolling
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
Supersonic expansion flow of an ionized gas
O. Igra
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
