Open AccessBoundary Layer Transition Preflight Experiments in a Mach-6 Quiet Tunnel
Author(s) -
Gregory McKiernan,
Brandon C. Chynoweth,
Steven P. Schneider,
Dennis C. Berridge,
Bradley M. Wheaton
Publication year - 2020
Publication title -
journal of spacecraft and rockets
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.758
H-Index - 79
eISSN - 1533-6794
pISSN - 0022-4650
DOI - 10.2514/1.a34772
Subject(s) - mach number , quiet , boundary layer , angle of attack , laminar flow , wind tunnel , laminar turbulent transition , turbulence , mechanics , swept wing , supersonic wind tunnel , stanton number , instability , water tunnel , airspeed , aerospace engineering , flow (mathematics) , physics , meteorology , aerodynamics , reynolds number , vortex , engineering , quantum mechanics
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