1.
A Spark Discharge Method for Measuring Flow Velocity and Moving Shock Mach Number in Low Density Flow Field
测量低密度气流速度和运动激波马赫数的火花放电法
2.
Effects of Mach Number on Surface Features of Interaction Between Swept Shock and Turbulent Boundary Layer
马赫数对后掠激波和湍流边界层干扰特性的影响
3.
Mach front
马赫锋[阵面, 波前]
4.
SIMPLE DISPOSAL OF MACH REFLECTION OF SPHERICAL SHOCK WAVE ON A PLANE
球面激波对平面的马赫反射的简化处理
5.
On transition criterion of Mach stem deformation for Mach reflections of pseudosteady strong shock waves
准定常强激波反射马赫杆突出变形准则的探讨
6.
On the Shape of Shock Waves in Steady Planar and Axisymmetical Mach Reflections;
平面与轴对称定常激波马赫反射中的激波形状研究
7.
Mach-Zehnder-Interferometer-A New Tuning Element for CW dye Laser
连续波环形腔染料激光器新的调谐元件——马赫-泽德干涉仪
8.
Study on Mach 4 internal flow with pseudo-shock waves using liquid crystal visualization method
液晶显示方法研究管内马赫数4拟似冲击波流动
9.
The point at which the incident wave, reflected wave, and Mach fronts meet is called the "triple point".
入射冲击波、反射冲击波与马赫波波阵面汇合之点叫做“三相点。”
10.
An aircraft instrument that indicates speed in Mach numbers.
马赫表装于飞机上的一种以马赫数来显示速度的仪器
11.
Mach limit altitude
马赫数受限制的飞行高度
12.
Empirical results are needed in the transonic Mach regime.
在跨音速马赫数范围内需要经验结果。
13.
The main flow is approximately dependent only on Mach number.
主流仍然近似地只同马赫数有关。
14.
③height H=11000m, Mach number M=1.4, attack angle α=0, sideslip angleβ = 10 deg.
③高度11000米,马赫数为1.4,10侧滑角。
15.
②height H=11000m, Mach number M=1.4, attack angle α = 10deg, sideslip angle β=0;
②高度11000米,马赫数为1.4,10度攻角;
16.
Implicit algorithms for viscous flow simulation at arbitrary Mach number
计算全马赫数下粘性流动的隐式算法
17.
Experimental study on the vortex tubes with different Mach number nozzles
喷嘴马赫数对涡流管性能影响的实验
18.
Investigation Electron Transport in Terahertz Quantum Cascade Laser and Waveguide;
太赫兹量子级联激光器电子输运及波导研究