mach cone

mach cone的基本解释

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马蒜锥

与mach cone相关的网络例句 [注：此内容来源于网络，仅供参考]

It is shown that maximum temperature value of the field's will rise while the Mach number increases. After the Mach number exceeds one, a clear bowshock is obtained in the simulation result, and the Mach angle decreases along with the Mach number. Those are consistent with theoretical results. While the Mach number is 3.5, even the radome inside is adiabatic, the maximum temperature is below 1000K. So the CVD diamond thick film radome can meet practical requirement of flight at 3.5 Mach number.

研究发现，随着马赫数的增加，温度场中最大温度值也随之增大；在马赫数大于1时，会产生明显的弓形激波，且激波的锥角随马赫数增加而减小，这与理论结果相一致；当马赫数为3.5时，即使在头罩内壁绝热条件下，温度场中最高温度值也在1000K以下，表明CVD金刚石厚膜可以满足Ma=3.5的实际飞行要求。

The following are the main objections with some real foundation:(1) The campaign of Lysias, which I Mach., iv, 26-34, places in the last year of Antiochus Epiphanes, is transferred in II Mach., xi, to the reign of Antiochus Eupator;(2) The Jewish raids on neighbouring tribes and the expeditions into Galilee and Galaad, represented in I Mach., v, as carried on in rapid succession after the rededication of the temple, are separated in II Mach.

以下是主要的反对与一些真正的基础：（ 1 ）的运动Lysias ，我马赫。，四， 26-34 ，地方在过去的一年里的安提阿哥伊皮法尼斯，是在二转马赫。，十一，对在位安提阿哥Eupator ；（ 2 ）以色列袭击邻国部族和探险到加利利和Galaad ，代表我马赫。，五，为迅速进行继承后重新庙宇，是分开的二马赫。

We then add boundaries delineated forward/backward facing reflected shock, Mechanical equilibrium, M2=1 and reflected shock strong/weak separating conditions on the (M0,q1) map of shih(2004). This is followed by systematically investigating multiply possible three shock theoretical solutions of steady Mach reflections in perfect triatomic gases. Pressure-deflection shock polar solutions are used to help illustrate different solution behaviors of these theoretical three-shock solutions. M0 is flow Mach no. upstream of incident shock, M1 is flow Mach no. downstream of incident shock, M2 is flow Mach no. downstream of reflected shock,q1 is flow deflection downstream of incident shock.

随后本文由石(2004)论文中加入前后分界、机械平衡、M2=1及强弱分界条件，然后有系统地探讨三原子分子理想气体(r=1.2857 )稳态马赫反射参震波理论多重解之交点及其对应之压力-转折角震波极图解，并建构出此三原子分子理想气体稳态马赫反射流场三震波十阶多项式理论解於(Mo，q1)平面上之解域图，其中M0为入射震波上游流场马赫数，M1为入射震波下游流场马赫数，M2为入射震波下游流场马赫数，q1为入射震波下游流场转折角。

与mach cone相关的网络解释 [注：此内容来源于网络，仅供参考]

Mach cone：马赫锥

mach angle 马赫角 | mach cone 马赫锥 | mach number 马赫数

Mach cone：马蒜锥;马赫锥

mach angle 马蒜角 | mach cone 马蒜锥;马赫锥 | mach criterion 马赫判据

Mach cone：麻克锥

麻克锥 Mach cone | 麻克波峰 Mach front | 麻克数 Mach number

Mach cone：马赫锥,扰动锥

Mach angle 马赫角 | Mach cone 马赫锥,扰动锥 | Mach diamond 菱形激波

edge of Mach cone：马赫[扰动]锥母线

taballa 片剂 | edge of Mach cone 马赫[扰动]锥母线 | collagenase [生化]胶原酶