delta-wing

基本解释

A variant of the swept-back wing is the delta wing.
后掠翼的变型是三角翼。
The canard surface, unlike a conventional tailplane which it replaces in delta wing designs, generates positive lift.
与三角翼所取代的常规布局中的尾翼不同，这种鸭翼是能产生正升力的。
The micro shear stress sensor which based on the smart skin for boundary-layer separation point detection of delta wing has been explored in this paper.
本文就以用于实现三角翼边界层分离点检测的面向灵巧蒙皮的微型剪应力传感器为对象展开研究。
The unsteady transonic flows around a pitching slender delta wing are simulated numerically with solving unsteady compressible Navier-Stokes equations by implicit finite difference TVD scheme.
用有限差分法求解N-S方程，数值模拟了细长三角翼作匀速上仰运动时的跨声速绕流流场。
NACA0012, NACA4412, RAE2822 airfoil and ONERA M6 wing, delta wing, slender body of missile and TND-712 wing-body standard model were chosen to confirm the validity of the current multigrid method.
选用了NACA0012翼型、NACA4412翼型、RAE2822翼型、ONERA M6机翼、大后掠三角翼、细长旋成导弹体及TND-712翼身组合体等多个算例对本文使用的多重网格方法进行了验证。