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Volumn , Issue , 2002, Pages
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Simulation of spinningmissile flowfields using U2NCLE
a a a |
Author keywords
[No Author keywords available]
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Indexed keywords
ANGLE OF ATTACK;
AXIAL FLOW;
MISSILES;
NAVIER STOKES EQUATIONS;
VERTICAL STABILIZERS;
VISCOUS FLOW;
AERO-DYNAMIC PERFORMANCE;
GRID RESOLUTION;
MOMENT COEFFICIENT;
NAVIER STOKES SOLUTION;
REFINEMENT GRIDS;
SEPARATED FLOWS;
SPINNING MISSILES;
VISCOUS CONTRIBUTIONS;
VORTEX FLOW;
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EID: 85067317513
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.2514/6.2002-2797 Document Type: Conference Paper |
Times cited : (10)
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References (7)
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