Yaw Angle Effect on Flow Structure over the Nonslender Diamond Wing

摘要

DELTAwings have evolved over the years and are primarily usednon many fighter aircraft. As these aircraft become more andnmore maneuverable, delta-wing vortex dynamics and the under-nstanding of the physics of time-dependent unsteady flows havenbecome substantially important [1]. Several variables affect the delta-nwing vortex dynamics. As indicated by Yaniktepe [2], some of thesenvariables are angle of attack, leading-edge geometry,wing thickness,nsweep angle, Reynolds number, and freestream conditions.nspans such as butterflies and hawkmoths.