1.
Numerical Simulation of Atomization and Combustion Based on Supersonic Inlet-channel Diesel Spray;
超音速进气道燃油喷射雾化及燃烧数值模拟
2.
Cross-section design of a controllable hypersonic inlet. The research is being done at the Nanjing University of Aeronautics and Astronautics.
南京航空航天大学正在进行一个可控高超音速进气道断面设计研究。
3.
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
4.
Rotornet: A High-Performance Hypersonic Decelerator for Planetary Entry
叶轮网,进入轨道用的高性能超音速减速器
5.
trisonic aerodynamics
三音速(亚音速、跨音速 、超音速)空气动力学
6.
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
7.
Numerical Simulation of Supersonic Axisymmetric Inlet Flow Field
超声速轴对称进气道流场的数值模拟
8.
extreme high-speed gas dynamics
高超音速气体动力学
9.
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
10.
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
11.
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
12.
transsuper aerodynamics
跨音速和超音速空气动力学
13.
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
14.
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
15.
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
16.
Investigation of a Two-dimensional Mixed-compression Hypersonic Inlet
一种高超声速二元混压式进气道的研究
17.
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
18.
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