vertical-tail

基本解釋

The sideslipping airplane gives rise to a side force on the vertical tail.
側(cè)滑的飛機(jī)在垂直尾翼上引起側(cè)力。
The vertical tail is less affected by the remainder of the airplane.
垂尾受飛機(jī)其它部分的影響較
The vertical tail size is not set to avoid spiral instability because this mode is not critical.
垂尾的大小不是根據(jù)避免螺旋不穩(wěn)定來確定的。因?yàn)檫@種運(yùn)動(dòng)模態(tài)不是設(shè)計(jì)狀態(tài)。
A multiblock patched grid for a modern twin vertical tail fighter and a domain decomposition solution of the Euler equation are given.
給出了一種生成現(xiàn)代雙立尾戰(zhàn)斗機(jī)外形的分區(qū)對(duì)接網(wǎng)格和Euler方程分區(qū)解。
It uses the same J-85 engine as its propulsion system but has a twin, outwardly canted vertical tail similar to the Boeing F/A-18.
它使用相同的J-85發(fā)動(dòng)機(jī)當(dāng)做它的動(dòng)力但是雙發(fā)飛機(jī)，機(jī)身上的傾斜垂尾類似波音F/A-18。