aerodynamic load distribution

基本解釋

The finite volume method was used to compute the aerodynamic load, and the effect of leading-edge cut and ribs on the pressure distribution was analyzed simultaneously.
使用有限躰積法計(jì)算了飛行時(shí)的氣動(dòng)載荷，分析了前緣切口和翼肋開孔對(duì)壓強(qiáng)分佈的影響；
A new free wake method is developed to calculate the convergent wake structure and blade aerodynamic load distribution. Computation results are compared to the experimental data.
發(fā)展了一種新的自由渦尾跡結(jié)搆計(jì)算方法，該方法能快速得到收歛的尾跡結(jié)搆，能比較準(zhǔn)確地計(jì)算槳葉載荷分佈。