low aspect-ratio

基本解釋

Numerical calculation and comparison are executed on two wings, one was an all-moved rudder, another was a low aspect-ratio wing with root fixed.
對(duì)某高超聲速全動(dòng)舵面和小展弦比根部固支翼面進(jìn)行了熱顫振的分析與比較。
Most low aspect-ratio flying wings have several redundant control surfaces, and the control allocation leads to the need to modify of some existing criterions.
由于可控性的設(shè)計(jì)要求需采用多操縱面的組合操縱，控制分配技術(shù)導(dǎo)致某些現(xiàn)有的品質(zhì)準(zhǔn)則需要修改。
hkxb.buaa.edu.cn
The directional axis flying qualities of low aspect-ratio combat flying wings were assessed in accordance with MIL—STD—1797A, and the evaluation results indicate the following aspects.
依據(jù)MIL—STD—1797A飛行品質(zhì)規(guī)范，對(duì)小展弦比飛翼布局作戰(zhàn)飛機(jī)的偏航軸飛行品質(zhì)進(jìn)行了評(píng)定研究。