NUMERICAL STUDY OF SHOCK GENERATION AT THE AFTER-BODY OF SLENDER BODY OF REVOLUTION USING NAVIER-STOKES EQUATION
24th, International congresss of aeronautical sciences ; 2004 ; Yokohama, Japan
2004-01-01
ICAS 2004-2.7.R.1
Also known as ICAS 2004.; HELD ON CD-ROM
Aufsatz (Konferenz)
Englisch
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Asymmetric vortices on a slender body of revolution
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|Asymmetric vortices on a slender body of revolution
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