音速的

F-15E Strike EagleThis jet, with its two huge afterburning turbofan engines, shakes the ground as it flashes by, just above the runway and just below the speed of sound.

的F - 15 E罢工eaglethis射流，与它的两个巨大的加力涡扇发动机，摇了摇地面，因为它闪烁，刚刚超过跑道和仅低于音速。

In this paper, aerodynamic optimization design of transonic wing is carried out by combination of optimization method with aerodynamic analysis of wing.

把最优化方法与机翼的气动力求解相结合，进行跨音速机翼的气动优化设计。

Fluent also provides a coupled solution method designed to deliver robust convergence performance for transonic flows.

流利还提供了一个耦合解决方法旨在提供强有力的收敛性能的跨音速流动。

On the other formed, polynomial expressions of intersected point between solution curves of WuestII, reflected shock backward-facing sonic, reflected shock backward-strong/weak separating, Mechanical equilibrium are derived and computed results are marked on the (M0,q1) theoretical solution map of perfect triatomic gas steady Mach reflection.

最后吾人针对WuestII曲线、后向音速曲线、后向强弱曲线、机械平衡曲线，推导它们之间的交点解公式，并将计算的结果标示於平面上之解域图上。

A spider may come with Web which ensnares their target while another may come with poison or a sonic attack - it's the luck of the draw.

一只蜘蛛可以拥有陷阱技能，而另一只可能拥有下毒或者音速攻击的技能。丫丫的，太强了。看来当猎人也不错。

Music A style of music evolved from southern Black American secular songs and usually distinguished by slow tempo and flatted thirds and sevenths.

蓝调音乐，布鲁斯：一种源于美国南部黑人通俗歌曲的音乐风格，通常表现为音速低缓，演奏第三和第七音节的降音调

The transonic flutter characteristics are investigated for several wings, empennage and wing-body configuration, flutter critical speeds are numerically simulated.

以ONERA M6机翼和无后掠矩形机翼为算例，分别对它们的跨音速定常和非定常粘性绕流进行了数值模拟，计算结果和有关文献的结果进行了比较，吻合较好。

Purpose-The study of the aspirated inflator on side airbag modulus can provide a new direction for airbag design. The main purpose of this project is to design, model and test a new inflator.

本研究主要在提供一个新的安全防护气囊基本构型品的设计方向，应用计算体学值方法模拟分析同几何尺寸气体产生器之近音速或超音速流场状态。

At first, a simple algebraic method is appied to generated O-H type three dimensional meshes, then the meshes are devided into tetrahedra meshes.

首先应用一种简单的代数方法生成了O-H型网格，然后，将其剖分为四面体网格，从而完成了简化航天飞机跨音速绕流的数值模拟。

With high temperature and high pressure in nozzle of wind tunnel, the effect of variable specific heat on nozzle design must be considered.

本文针对超音速、高超音速喷管内马赫数、温度变化剧烈的特点，研究了比热容变化对设计喷管型面产生的影响。

The split between the two groups can hardly be papered over.

这两个团体间的分歧难以掩饰。

This approach not only encourages a greater number of responses, but minimizes the likelihood of stale groupthink.

这种做法不仅鼓励了更多的反应，而且减少跟风的可能性。