机译:接近固体表面的超音速弹丸的空气动力学
University of New South Wales, Sydney, New South Wales 2052, Australia;
rnUniversity of New South Wales, Sydney, New South Wales 2052, Australia;
rnUniversity of New South Wales, Sydney, New South Wales 2052, Australia;
rnUniversity of New South Wales at the Australian Defence Force Academy, Canberra, Australian Capital Territory 2600, Australia;
rnUniversity of New South Wales at the Australian Defence Force Academy, Canberra, Australian Capital Territory 2600, Australia;
C_(DA): drag force coefficient in the x-direction, based on projected frontal area; C_(Mx): lateral moment coefficient; C_(Ma): pitching moment coefficient; C_(Na): force coefficient acting normal to the ground plane, based on projected side area; C_P: pressure coefficient; et al;
机译:接近固体表面的超音速弹丸的空气动力学
机译:推进器元件引起的表面缺陷对超音速弹丸空气动力学的影响
机译:从亚音速到超音速的非定常空气动力学计算和马格努斯效应对旋转弹丸计算轨迹的影响
机译:超音速弯曲弹丸的气动形状优化
机译:用于提升表面的超音速非稳态空气动力学的新的加速势方法,非平面超音速双重点方法的进一步扩展以及用于超音速,瞬态响应非稳态空气动力学的非线性,非梯度优化有理函数逼近。
机译:巨大射弹冲击对固体的光子发射
机译:超音速二维制导炮弹的气动参数优化设计
机译:基于矢量评估遗传算法的超音速弯曲弹体气动优化。