1) forward-swept wings
前掠机翼
2) swept-leading-edge wing
前缘后掠机翼
3) forward swept wing
前掠翼
1.
The divergence experiment prediction techniques of flat plate forward swept wings are presented.
介绍了平板前掠翼的发散试验技术。
4) forward-swept wing
前掠翼
1.
The W-shaped tailless aircraft has not stabilizer and vertical tail,and it is based on the design of forward-swept wing and the integrated design of blended wing-fuselage.
W型无尾飞机基于前掠翼及翼身融合的一体化设计,取消了平尾和垂尾,可大幅降低雷达反射截面积,减轻结构重量;同时具有亚声速气动效率高、横航向操纵面效率高的优势。
2.
The authors investigate experimentally the effect of canard wing and sweep angle on longitudinal aerodynamic characteristics of canard-forward-swept wing configuration by means of forces measurement in wind tunnel.
前掠翼布局由于其潜在的优势,在未来战斗机的研制中将占有日益重要的地位。
3.
Its design idea is based on the flow behavior of forward-swept wing and the flow control concept.
提出了一种新型的飞机气动外形—— W-型无尾布局及其气动设计思想 ,初步研究了两种气动布局方案 :前掠翼无尾气动布局和 W-型无尾气动布局。
5) variable forward-swept wing
变前掠翼
1.
The Unmanned Aerial Vehicle(UAV) with variable forward-swept wing is a new design concept,which integrates the advanced aerodynamic characteristics of orthogonal wing,delta wing and the forward-swept wing.
针对变前掠翼无人机设计了一种翼身连动机构,使无人机能够根据任务需求,在直机翼、前掠翼、三角翼之间进行气动布局转换,从而在整个任务飞行过程都能达到性能最佳。
2.
A new aerodynamic configuration of unmanned aerial vehicle (UAV) with variable forward-swept wing was investigated, under which the forward-swept angle can be varied to obtain optimal aerodynamic characteristics during low, subsonic, tansonic and supersonic speeds.
研究了一种新的变前掠翼无人机气动布局概念,在低、亚、跨和超声速状态下可通过改变机翼的前掠角来获取最佳的气动性能。
6) highly swept-back wing
大后掠机翼
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条