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Visualization of Supersonic Flow past EOS
Author(s) -
Ting C.C.
Publication year - 2001
Publication title -
zamm ‐ journal of applied mathematics and mechanics / zeitschrift für angewandte mathematik und mechanik
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.449
H-Index - 51
eISSN - 1521-4001
pISSN - 0044-2267
DOI - 10.1002/zamm.200108115161
Subject(s) - schlieren , supersonic speed , flow visualization , shock wave , shock (circulatory) , vortex , mach number , visualization , choked flow , mechanics , flow (mathematics) , angle of attack , physics , materials science , optics , geology , engineering , aerodynamics , mechanical engineering , medicine
The visualization of supersonic flow around EOS ]1[ involves analyzing shock wave positions and vortices at large angles of attack. The applied experimental methods include color Schlieren, oil film and vapor screen techniques. Depending on the Mach number and the angle of attack various vortex structures are observed on the leeward side.