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Volumn , Issue , 2003, Pages
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Toward enabling objective englneering designs for rocket injectors-efficient evaluation of larger design space via automated parametric grid generation
a a a a |
Author keywords
[No Author keywords available]
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Indexed keywords
COMPUTATIONAL FIELD SIMULATIONS;
CONCOMITANT REDUCTION;
CONVENTIONAL APPROACH;
DESIGN PARAMETERS;
GENERATION PROCESS;
GRID GENERATION;
INJECTOR GEOMETRY;
MULTI-BLOCK GRID;
DESIGN;
MESH GENERATION;
PROPULSION;
ROCKETS;
GEOMETRY;
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EID: 84897585312
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (3)
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References (6)
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