1.
Numerical Simulation of Supersonic Axisymmetric Inlet Flow Field
超声速轴对称进气道流场的数值模拟
2.
An Investigation of Stable Operation Range in Supersonic Axisymmetric Inlet
超声速轴对称进气道稳定工作范围研究
3.
Investigation of the Hypersonic Axis-symmetricail Vehicle s Aerodynamic Performance and Its Flow Performance of the Whole Flow Path;
高超声速轴对称飞行器气动力特性及其全流道流动特征的研究
4.
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
5.
Influence of blunted-lip cowl on performance of supersonic mixed-compression inlet
钝化唇缘对超声速混压式进气道性能的影响
6.
Effect of aspect ratio on 2-D hypersonic inlet performance
宽高比对二元高超声速进气道性能的影响
7.
Impact of suction position on starting of hypersonic inlet
抽吸位置对高超声速进气道起动性能的影响
8.
Performance and boundary layer of flow in axisymmetric mixed-compression supersonic inlet with cavity
槽对超声速混压式进气道性能及边界层的影响
9.
Numerical Simulation of External-Compression Supersonic Inlet Flow Fields
外压式超声速进气道流场的数值模拟
10.
Effects of wall temperature on unstart/restart characteristics of hypersonic inlets
壁面温度对高超声速进气道不起动/再起动特性的影响
11.
Effects of turning angles of wedge on unstart/restart characteristics of hypersonic inlets
楔面转折角对高超声速进气道不起动/再起动特性的影响(英文)
12.
Study of Inlets/body Aerodynamic Interference of Supersonic Tactical Missile Using Numerical Simulation;
超声速战术导弹进气道/弹身气动干扰数值研究
13.
Design and Experimental Verification of Hypersonic Inlet with Rectangular Section
矩形截面高超声速进气道气动设计及实验验证
14.
Numerical Simulation and Experiment of Integral Flow Field of Diverterless Supersonic Inlet/Forebody
无隔道超声速进气道/前机身一体化计算与试验
15.
Design and wind tunnel test of an axisymmetric inlet for ramjet engine
冲压发动机用轴对称进气道设计和试验
16.
Supersonic chin inlet/airframe integration design
超声速下颔式进气道/前机身一体化方案设计
17.
Numerical Simulation and Experimental Research of Hypersonic Inlet;
高超声速进气道流场数值模拟与试验研究
18.
Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet;
高超声速进气道的设计、计算与实验研究