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Volumn , Issue , 1992, Pages
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Supersonic jet mixing enhancement by “Delta-Tabs”
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Author keywords
[No Author keywords available]
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Indexed keywords
LAMINAR BOUNDARY LAYER;
MIXING;
NOZZLES;
PROPULSION;
TURBULENCE;
TURBULENT FLOW;
VORTEX FLOW;
MIXING LAYERS;
NOZZLE EXIT PLANE;
STREAMWISE VORTICES;
SUPERSONIC JETS;
TRIANGULAR SHAPES;
TURBULENCE INTENSITY;
TURBULENT BOUNDARY LAYERS;
VORTEX GENERATORS;
SUPERSONIC AERODYNAMICS;
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EID: 85005987252
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.1992-3548 Document Type: Conference Paper |
Times cited : (44)
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References (11)
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