考虑机身影响的三角翼跨音速气动力设计

TRANSONIC AERODYNAMIC DESIGN OF DELTA WINGS UNDERGOING BODY EFFECTS

将给定翼面目标压力分布的余量修正法（一种三维机翼气动力反设计方法）推广应用于考虑机身影响的小展弦比三角翼跨音速气动力设计。

An inverse aerodynamic wing design method by residual correction for prescribed pressure is extended to the aerodynamic design of delta wings undergoing body effects in transonic flow. The resolution of some difficulties about these design procedure is given by a body delta wing combination design example.