The researches of nonlinear finite element and experiment indicate that the effect of anti-shear which is aroused by the width of the joints' wing board.
通过试验以及非线性有限元研究发现：节点区翼缘板外伸宽度对节点抗剪性能的影响与梁柱抗弯刚度比有关。
The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
从全速位方程出发研究了机翼和翼身融合体跨音速绕流的有限元算法。
Abstract :Failure process of a primary load-bearing composite joint in wing root was analyzed by finite element methods, and the ultimate strength of the joint was predicted.
以复合材料机翼翼根后梁下缘条对接试件为研究对象，通过有限元手段分析其失效机理和破坏过程，并对极限强度进行预测。
The performance and flows of 2-D Wing-In-Ground Effect are numerically simulated by solving RANS equations using an implicit finite difference method.
本研究以隐式差分方法求解不可压RANS方程，对二维地效应翼的性能及周围流场进行数值模拟。
In this paper, technical data have been obtained precisely by computing and analyzing the structure of wing joint with finite element method.
通过对机翼接头结构的有限元分析计算，得到接头各部分的应力数值。
The calculating results of this method for the C-5A aircraft wing are fairly close to that of implicit finite-difference method using Cebecis algebraic turbulent model.
对C - 5a机翼的计算结果表明，该方法具有同微分方法可以比拟的计算精度。
The calculating results of this method for the C-5A aircraft wing are fairly close to that of implicit finite-difference method using Cebecis algebraic turbulent model.
对C - 5a机翼的计算结果表明，该方法具有同微分方法可以比拟的计算精度。
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