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RUNGE-KUTTA FINITE-VOLUME SIMULATION OF LAMINAR TRANSONIC FLOW OVER M6 WING USING THE NAVIER-STOKES EQUATIONS

Author(s):
MULLER, B. et al. ( RES. INST. OF NATL. DEFENCE, STOCKHOLM )  
Publication title:
NASA Technical Reports(N88-)
Pub. Year:
1987
Issue:
FFA-TN-1987-06
Paper no.:
N88-28045
Page(from):
1
Page(to):
46
Pages:
46
Pub. info.:
National Aeronautics and Space Administration
Language:
English
Type:
Technical Paper

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