COMPARISON OF STAGNATION PRESSURE CONTROL SYSTEMS FOR A 12-INCH BLOWDOWN TRANSONIC TUNNEL
Author(s) -
R.C. Maydew
Publication year - 1957
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/4328733
Subject(s) - transonic , boiler blowdown , mach number , stagnation pressure , wind tunnel , supersonic speed , supersonic wind tunnel , hypersonic wind tunnel , subsonic and transonic wind tunnel , stagnation temperature , aerospace engineering , stagnation point , engineering , mechanics , aeronautics , aerodynamics , mechanical engineering , physics , heat transfer , inlet
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