"Compressible flow." . . "Wind." . . "Test Facilities, Equipment and Methods." . . "Pressure." . . "(Skin friction." . . "Experimental data." . . "Fluid Mechanics." . . "Pressure gages." . . "Surface properties." . . . . . . . . . . . . . . . . . . . . "Surface impact pressure probe method of measuring local skin friction at supersonic speeds"@en . . . . . . . . . . . . . "The purpose of the report is to demonstrate, on the basis of wind tunnel results, the feasibility of using a surface probe. This phase is limited to thermally insulated surfaces with zero pressure gradient."@en . "Experimental investigation of the surface impact pressure probe method : of measuring local skin friction at supersonic speeds"@en . . "Experimental investigation of the surface impact pressure probe method of measuring local skin friction at supersonic speeds"@en . "Experimental Investigation of the Surface Impact Pressure Probe Method of measuring local skin friction at supersonic speeds"@en . "Experimental investigation of the surface impact pressure probe method of measuring local skin friction at supersonic speeds" . . "DEFENSE RESEARCH LAB UNIV OF TEXAS AUSTIN." . . "Probes." . . "Impact shock." . . "Supersonic flight)" . . "Boundary layer." . . . .