Euler technology assessment for preliminary aircraft design employing overflow code with muliblock structured-grid method

Contributor(s): Language: English Series: NASA CR 4651 : 1995Publication details: Washington, D.C. ; National Aeronautics and Space Adminstration ; 1995Edition: Description: 66 p; ISBN: Subject(s): | Computational fluid dynamics, Euler formulation,Preliminary aircraft design, Sharp-edge flow-separation, Vortex flowOnline resources: Click here to access online
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Item type Current library Call number Status Date due Barcode Item holds
Pamphlets Standards Reports Pamphlets Standards Reports Central Library, IITB
LNASA CR 4651 : 1995 Not for loan A62673
Total holds: 0

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