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Volumn , Issue , 2001, Pages
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Numerical investigation of compressibility effects on active control of boundary layer separation
a a |
Author keywords
[No Author keywords available]
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Indexed keywords
BOUNDARY LAYERS;
COMPRESSIBILITY;
LAMINAR FLOW;
NASA;
REYNOLDS NUMBER;
WIND TUNNELS;
BOUNDARY-LAYER SEPARATION;
COMPRESSIBILITY EFFECTS;
CRYOGENIC WIND TUNNELS;
EXPERIMENTAL RESEARCH;
FORCING FREQUENCIES;
HIGH-ORDER FINITE DIFFERENCES;
NASA LANGLEY RESEARCH CENTER;
NUMERICAL INVESTIGATIONS;
COMPUTATIONAL FLUID DYNAMICS;
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EID: 85086615495
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.2001-2771 Document Type: Conference Paper |
Times cited : (3)
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References (15)
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