- 更多网络例句与跨音速的相关的网络例句 [注：此内容来源于网络，仅供参考]
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An improved engineering approach to flutter analysis of wings with high angle of attack is presented.
跨音速颤振分析是飞行器工程设计中至今未完全解决的关键技术之一。
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"Plateau Eagle" advanced trainer adopts the aerodynamic arrangement of double delta wings with high lift-drag ratio, the leading edge of outside wing rotated conically and air inlet beneath both sides ribs, and has a good take-off/landing performance and subsonic/transonic speed performance in medium-low altitude.
"山鹰"高级教练机采用高升阻比双三角机翼气动布局，外翼前缘锥形扭转以及两侧肋下进气道，具有良好的起降性能和中低空亚跨音速性能。
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And with this method, an implicit difference equation for solving the unsteady transonic flow with Euler equations is established.
在此基础上建立了可用于跨音速非定常流动的Euler方程隐式求解法。
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In this paper,the transonic two dimensional airfoil integral equation given by Nixon [1,2,3] has been extended to three dimensional thin wing case.
本文将Nixon[1，2，3]对二维薄翼型所建立的跨音速积分方程推广到三维薄机翼情况。
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In the computation of aerodynamic forces, the present work is based on the work of Morino et al., but the following aspects are improved:(1) In computing the steady transonic aerodynamic load, the steady transonic nonlinear integral equation is solved by relaxation-iteration method in this thesis, instead of solving the time dependent transonic nonlinear integral equation, so that the computing time is saved greatly;(2) The influence coeifficients represented by volume integral are transformed to surface integral by using the Gaussian Theorem, so the analytical form of these coeifficients can be obtained and this leads to be more convenient to analyse and compile computer program;(3) The shock capturing method is used in every time step in present work, no shock moving term is added in the integral equation, so that it is more convenient and simpler to treat.
在气动力计算方面，本文基于Morino等人的工作，作了如下几方面的改进：（1）在计算定常跨音速流场（作为非定常绕流计算的初场）时，本文采用松驰迭代法直接求解跨音速定常非线性积分方程，而不是采用时间相关法求解非定常非线性积分方程，这样大大节省了计算机时；（2）将以体积分形式出现的影响系数化为面积分，并获得解析公式，这样便于分析和编写程序；（3）对运动的激波，本文通过在每一个时间步长上采用激波捕捉法而得到，而不是在积分方程中附加激波运动项，因而处理起来简单方便得多。
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Use pattern of Gao-Yong compressible onflow, 2 dimension of numeric imitate RAE2822 wing section differs in two kinds will shed what the circumstance falls to cross velocity of sound agglutinant circle sort a problem.
梗概： 应用Gao-Yong可压缩湍流模式，数值模拟RAE2822二维翼型在两种不同来流情况下的跨音速粘性绕流新问题。
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In the meantime, mutual to shock wave of wing section surface and attrib border layer interference and turn turn problem undertakes analytic computation, the result makes clear, the numeric method with proper union of mode of Gao-Yong compressible onflow can succeed ground imitate wing section steps sonic and agglutinant flow.
同时，对翼型表面激波和边界层相互干扰以及转捩新问题进行分析计算，结果表明，Gao-Yong可压缩湍流模式结合适当的数值方法能够成功地模拟翼型跨音速粘性流动。
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Jameson's rotated difference algorithm is investigated with the aid of the orthogonal stream-lines coordinate system.
以正交流线坐标系为工具，考察了求解跨音速流动的Jameson旋转差分格式。
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The isentropic efficiency of the optimum design has 1.59% higher than that of the reference design.
完成了小展弦比跨音速透平级的气动优化设计。
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On the basis of simulating unsteady viscous flows, coupling the structure dynamics equations, the problem of flutter is investigated for wings, empennage and wing-body configuration.On the basis, many examples, simulating the steady and unsteady viscous flows around wings, are given in this paper.
在模拟非定常粘性绕流的基础上，与颤振运动方程相耦合，分别对机翼、尾翼和组合体流固耦合现象中颤振问题进行了研究，准确求解跨音速颤振临界速度，分析它们在跨音速范围的颤振规律，并研究分析了机翼剖面形状变化对颤振速度的影响。
- 更多网络解释与跨音速的相关的网络解释 [注：此内容来源于网络，仅供参考]
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transoceanic communication：越洋通信,海外通信
"transmutation product ","转化产物,蜕变产物" | "transoceanic communication ","越洋通信,海外通信" | "transonic ","跨音速的,超音速的"
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Transpacific Westbound Rate Agreement：越太平洋西行运费率协定
transonic 跨音速的 | Transpacific Westbound Rate Agreement 越太平洋西行运费率协定 | transpacific 横渡太平洋的
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transonic：跨音速
物体只有一些部份(例如转子叶片的末梢)其周遭空气是超过音速的情形称为跨音速(transonic);出现这种情况,常见的物体速度值是介于0.8马赫与1.2马赫之间.
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transonic nozzle：跨音速喷管
transfer crane 运送吊车,搬运吊车 | transonic nozzle 跨音速喷管 | transport crane 运输起重机,运输用的起重机
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transonics：跨音速空气动力学
transonic /接近音速的/ | transonics /跨音速空气动力学/ | transosonde /平移探空仪/越空探测/
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transsonic：跨音速的
transsmissivity 透射率 | transsonic 跨音速的 | transtainer 桥式集装箱换装起重机