This paper deals with the numerical methods for transonic flows around airfoil and wing, and its applications.

本論文研究翼型和機(jī)翼跨音速定常流的數(shù)值方法及其應(yīng)用方面的問題，主要的工作是

And with this method, an implicit difference equation for solving the unsteady transonic flow with Euler equations is established.

在此基礎(chǔ)上建立了可用于跨音速非定常流動(dòng)的Euler方程隱式求解法久久avabb。

Thus it was extensively applied to experimental research of transonic and hypersonic flow.

因此粉色视频又黄又爽免费，它在跨聲速和超聲速流的實(shí)驗(yàn)研究中得以廣泛地應(yīng)用。

Suitable for numerical simulation of subsonic毛片无码午夜国产视频、transonic and supersonic flow field of nozzle.

3適應(yīng)于噴管內(nèi)亞免费的一级毛片、跨、超音速流場(chǎng)的數(shù)值模擬什么视频可以看毛片。

The numerical method for the unsteady transonic flow is presented in the third part of this thesis.

在第三部分中午夜影院三级，根據(jù)前面所提出的求解Euler方程的方法91精品视频网，利用非定常問題的邊界條件91页国产视频，建立了計(jì)算跨音速非定常流動(dòng)的計(jì)算方法。

transonic aerodynamics：跨聲速空氣動(dòng)力學(xué)

transonic 跨聲速的 | transonic aerodynamics 跨聲速空氣動(dòng)力學(xué) | transonic flow 跨聲速憐

transonic aerodynamics：穿音速空氣動(dòng)力學(xué)

transmutation 衰變 | transonic aerodynamics 穿音速空氣動(dòng)力學(xué) | transonic aircraft 穿音速飛機(jī)

transonic：跨音速

物體只有一些部份(例如轉(zhuǎn)子葉片的末梢)其周遭空氣是超過音速的情形稱為跨音速(transonic);出現(xiàn)這種情況,常見的物體速度值是介于0.8馬赫與1.2馬赫之間.

transonic：穿音速

航太術(shù)語(yǔ)中慣用次音速(subsonic),穿音速(transonic),超音速(supersonic)超高音速(hypersonic)來區(qū)分飛機(jī)飛行的速度航太術(shù)語(yǔ)中慣用次音速(subsonic),穿音速(transonic),超音速(supersonic)超高音速(hypersonic)來區(qū)分飛機(jī)飛行的速度

transonic：跨聲速的

嬗變,銳變 transmutation | 跨聲速的 transonic | 跨聲速效應(yīng) transonic effect