1.
NUMERICAL CALCULATION WITH FINITE DIFFERENCE METHOD FOR SUPERSONIC FLOW OVER BENT CONES
绕弯曲头锥超音速流动差分法数值计算
2.
Numerical Analysis of Aero-optic Effects Induced by the Turbulence Flow Field Surrounding Super/Hypersonic
超音速/高超音速飞行器湍流流场气动光学效应分析
3.
Study on the Rotating Supersonic Condensing Flow and Application Technology
旋转超音速凝结流动及应用技术研究
4.
Aero-Optic Effects Induced by the Fluctuation Flowfield Surrounding Hypersonic Aircrafts
超音速湍流脉动流场气动光学效应分析
5.
trisonic aerodynamics
三音速(亚音速、跨音速 、超音速)空气动力学
6.
Gas-particle Two Phase Flow in Supersonic Cold Gas Dynamic Spray;
超音速冷气体动力喷涂过程中的气固两相流动
7.
Aerodynamic flutter and limited cycle of a 2-D wing in the supersonic flow field
超音速流中二元机翼的气动颤振与极限环
8.
Pulsation response of a two dimensional wing to atmosphere turbulence in supersonic flow
大气紊流作用下超音速二元机翼的脉动响应
9.
SHOCK EFFECT IN SUPERSONIC NON-EQUILIBRIUM CONDENSING STEAM FLOW
水蒸气超音速非平衡凝结流动中的激波效应
10.
extreme high-speed gas dynamics
高超音速气体动力学
11.
ultrasonically activated extruder
超音速驱动的挤压机
12.
transsuper aerodynamics
跨音速和超音速空气动力学
13.
The numerical simulating of the supersonic gas-particle two phase flow in De-Laval-Nozzle;
冷气体动力喷涂喷管内超音速气固两相流动数值模拟
14.
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
15.
In conclusion we note the following general items concerning flow in supersonic nozzles.
最后，我们归纳几个关于超音速喷管流动的一般原则。
16.
AN EXPERIMENTAL STUDY OF HELIUM INJECTION WITH AN AERODYNAMIC RAMP INJECTOR IN SUPERSONIC FLOW
超音速空气流中气动斜坡喷嘴喷射氦的实验研究
17.
THE EFFECT OF RATE OF EXPANSICN ON THE CONDENSATION OF SUPERSONIC WET STEAM FLOW IN A LAVAL·NOZZLE
膨胀率对拉伐尔喷管超音速湿蒸汽流动凝结过程的影响
18.
The Blowing-off of the Lip Separation of an Axisymmetric Supersonic Inlet and the Analysis of the Coherence of Dynamic Distortion of the Inlet
超音速轴对称进气道唇口分离流吹除及其动态畸变源相干分析