Corner flow

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 and W.W. Liou.

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

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

Supersonic expansion flow of an ionized gas

O. Igra.

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, Royce D. Moore and Rickey J. Shyne.

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

Awatef Hamed, principal investigator.

Stability of the laminar boundary layer in a streamwise corner

by William D. Lakin.

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

Birinchi Hazarika and Rishi S. Raj.

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction: final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95

David S. Dolling and J.W. Barter.

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, Royce D. Moore, Rickey J. Shyne and Donald R. Boldman.