As an innovative aircraft configuration , its essence is the integration of aerodynamics and structure 作為一種飛行器創(chuàng)新布局,其本質(zhì)是氣動(dòng)/結(jié)構(gòu)一體化的布局形式。
Improving system decomposition method for application to multi - objective optimization of aircraft configuration design 的系統(tǒng)分解法及其在飛行器外形優(yōu)化設(shè)計(jì)中的應(yīng)用
Investigation of integrated multi - disciplinary and multi - objective optimization of the aircraft configuration design method 飛行器外形多目標(biāo)多學(xué)科綜合優(yōu)化設(shè)計(jì)方法研究
For advanced tactical fighter , besides excellent aerodynamic performance , stealthy performance is an important factor for aircraft configuration design 先進(jìn)戰(zhàn)斗機(jī)除了具有優(yōu)良的氣動(dòng)特性外,隱身性能也已經(jīng)成為其外形設(shè)計(jì)的重要因素。
The deep - stall characteristics of different aircraft configurations are analyzed with bifurcation analysis methods , and the convergence regions of a deep - stall attractor are constructed with backward integration techniques 摘要用分支分析方法分析了不同構(gòu)型飛機(jī)的深失速特性,用反向積分技術(shù)計(jì)算了深失速吸引子的吸引域。