Open AccessAnalytical and experimental heat transfer and flow-field prediction on a rectangular reentry module
Author(s) -
A. LAGANELLI
Publication year - 1980
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/6087747
Subject(s) - reentry , hypersonic speed , mechanics , mach number , wind tunnel , heat transfer , convective heat transfer , inviscid flow , space shuttle thermal protection system , bow shock (aerodynamics) , aerospace engineering , shock (circulatory) , hypersonic wind tunnel , flow (mathematics) , supersonic speed , angle of attack , expansion tunnel , physics , meteorology , aerodynamics , thermal , shock wave , engineering , medicine , cardiology
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