25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS2006-3.2S

IMPACT OF MODEL PLUNGING MOTION ON WIND TUNNEL WALL PRESSURE FLUCTUATIONS

A. R. Davari, M. R. Soltani*, A. Mohammadi
Azad Univ., Iran; *Sharif Univ., Iran

Keywords: plunging motion, tip vortex, induced velocity, steady flow

In this paper, the wind tunnel wall pressure fluctuations have been measured during a plunging motion of a standard Fighter type configuration model. Effects of angle of attack and oscillation frequency were studied on wall pressure time history

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