Open AccessWind Tunnel Study of Probes for Measuring Pressure Fluctuations on an Ablative Hypersonic Reentry Vehicle
Author(s) -
H. Heller
Publication year - 1967
Publication title -
the journal of the acoustical society of america
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.619
H-Index - 187
eISSN - 1520-8524
pISSN - 0001-4966
DOI - 10.1121/1.2144251
Subject(s) - hypersonic speed , heat shield , hypersonic wind tunnel , wind tunnel , space shuttle thermal protection system , supersonic speed , reentry , flow (mathematics) , aerospace engineering , mechanics , boundary layer , supersonic wind tunnel , ablation , acoustics , materials science , physics , meteorology , thermal , engineering , medicine , cardiology
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