1.
Unlike in subsonic and transonic speed regimes, the interference resulting from the finite size of the test region is seldom present.
不像在亚、跨音速区域，这里因试验段尺寸有限造成的干扰是难得存在的。
2.
trisonic aerodynamics
三音速(亚音速、跨音速 、超音速)空气动力学
3.
transsuper aerodynamics
跨音速和超音速空气动力学
4.
Stability of Transonic Shocks in Supersonic Flow Past a Wedge;
超音速绕流中产生的跨音速激波的稳定性研究
5.
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。
6.
NUMERICAL INVESTIGATION OF FLOW FIELD IN A 1.5-STAGE TRANSONIC COMPRESSOR
1.5级跨音速压气机内部流场数值分析
7.
Gridless Method for the Simulation of Transonic and Supersonic Flows;
无网格方法在跨音速、超音速流场数值模拟中的应用
8.
THE AERODYNAMIC PERFORMANCE COMPUTATION OF WINGS USING TRANSONIC FULL POTENTIAL EQUATION
跨音速全位势方程的机翼气动性能计算
9.
Transonic Unsteady Aerodynamics and Flutter Computations for Complex Assemblies;
复杂组合体跨音速非定常气动力和颤振计算
10.
Credibility Analysis of RAE2822 Airfoil Transonic Flow Computation
RAE2822翼型跨音速流动CFD计算的可信度分析
11.
Numerical Research on Effects of Splitter Blades on a Transonic Centrifugal Compressor Impeller
跨音速离心压缩机叶轮分流叶片的数值研究
12.
The Application of Transonic Velocity Potential Equation with Higher Order Approximation for Computing the Pressure Distribution over the Blunt Leading-edge Airfoil
应用跨音速高级近似扰动速势方程计算钝前缘翼型的压力分布
13.
An integral boundary layer method based on the dissipation integral is used to account for viscous effects.
考虑附面层影响，通过粘/迭代得到跨音速翼/的非定常气动力。
14.
VARIATIONAL PRINCIPLE WITH VARIABLE DOMAIN DISCO-NTINUOUS FINITE ELEMENT METHOD FOR TRANSONICFLOW AND DETERMINING AUTOMATICALLY THEPOSITION AND SHAPE OF THE SHOCK WAVES
跨音速流场的变域变分间断有限元解法及激波位置的自动捕获
15.
The aerodynamic force is solved with the second order approximation method for transonic small disturbance potential flow.
用跨音速小扰动势流的二级近似方法求解气动力;
16.
《Finite Difference Computations of Pressure and Wave-Drag of Slender Bodies of Revolution at Transonic Speed with Zero-Lift》
跨音速细长旋转体零升力时的压力和波阻力的有限差分计算
17.
Prediction and Analysis of Fluctuating Pressure at Transonic Mach Numbers and Nonlinear Characteristic of RB Convection System;
跨音速脉动压力及RB对流系统非线性特征的预测与分析
18.
Numeric Investigation of Using Endwall Fences in Annual Cascade of Transonic Compressor;
跨音速环形压气机叶栅中应用翼刀技术的数值研究