25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS2006-2.5S

COMPUTATIONAL ANALYSES OF SUPERSONIC FLOWS OVER A DELTA WING AT HIGH ANGLES OF ATTACK

G. Imai, K. Fujii*, A. Oyama*
Univ. of Tokyo, Japan; *JAXA, Japan

Keywords: delta wing, supersonic flow, CFD, aerodynamic characteristics, high angle of attack

Subsonic to supersonic flows over a delta wing at high angles of attack have been computationally investigated. The computational result revealed the three-dimensional flow structure over a delta wing at various flow conditions.

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