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by Devendra S. Parmar
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Skin-friction measurements in a 3-D, supersonic shock-wave/boundary-layer interaction
Aerospace Sciences Meeting & Exhibit (32nd 1994 Reno, Nev.)
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
Khaled S. Abdol-Hamid
Boundary-layer transition and global skin friction measurement with an oil-fringe imaging technique
Daryl J. Monson
Shock tunnel studies of scramjet phenomena 1994
R. G. Morgan
Shock tunnel studies of scramjet phenomena 1995
Instrumentation development for study of Reynolds analogy in reacting flows
Dianne J. DeTurris
Feasibility of generating an "artificial" burst in a turbulent boundary layer
Mohamed Gad-el-Hak
Evaluation of heated film sensors for the measurement of wall shear stress
Yves Drolet
Dual cylindrical wave laser-Doppler method for measurement of skin friction in fluid flow
Amir Ahmad Naqwi
