1.
Flow field calibration of NUAA Φ0.5m hypersonic wind tunnel
南航Φ0.5m高超声速风洞流场校测(英文)
2.
The Test and Calibration of Φ200 Hypersonic Wind Tunnel
Φ200高超声速风洞调试和流场校测
3.
Mach Number Seven and Eight Nozzle Design of the Diameter One Meter Hypersonic Wind Tunnel and Flow Field Testing;
Φ1米高超声速风洞M7、8喷管设计及流场校测
4.
The experimental results of low temperature ablator (beeswax and camphor) tests in the hypersonic wind Tunnel are presented in this paper.
本文给出了低温烧蚀材料的高超声速风洞烧蚀实验研究的结果。
5.
Development of Experimental Power Source and Temperature Control System for Φ1m Hypersonic Wind Tunnel;
Φ1米高超声速风洞加热器试验电源及温控系统设计
6.
The Design and Experimental Studies of Supersonic Straight Through Wind Tunnel and "Supersonic-supersonic" Mixing Layer Wind Tunnel;
直连式超声速风洞与“超—超”混合层风洞的设计和实验研究
7.
Hypersonic propulsion test facility is important for the scramjet ground tests.
高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
8.
Aero-Acoustic Experimental Investigation of the Cavity Flow Fields in High Speed Wind Tunnel;
高速风洞弹舱流场气动声学特性试验研究
9.
Experimental Investigation of Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Twin-inlet 90° Configuration at Venter
双下侧定几何二元混压式超声速进气道的风洞试验
10.
Analyses of High Altitude Wind Model of Hypersonic Flight Test
高超声速飞行试验风场建模与仿真分析
11.
A review of heat exchanger study for large-scale continuous transonic wind tunnels
大型连续式跨声速风洞热交换器概述
12.
Design of Ultrasonic Anemometer Measurement System with High Sensitivity Based on C8051F020
一种高精度超声波风速风向测量系统设计与研究
13.
An investigation of background noise measurement technology in aeroacoustic wind tunnel
低速航空声学风洞背景噪声测试技术研究
14.
Calculating Friction Velocity from Data by a Ship-borne Supersonic Anemometer;
由船载超声风速仪数据计算摩擦速度
15.
In compensation, the black hole is a much faster processor.
可资弥补的是，黑洞是个超高速处理器。
16.
Compressibility effects are investigated with highspeed models in high-speed tunnels.
压缩性影响需用高速模型在高速风洞中试验。
17.
Aerodynamic Flutter and Limited Cycle of a 2-D Wing in the Hypersonic/Supersonic Flow Field
超声速/高超声速流中二元机翼的颤振与极限环
18.
Hypersonic wind tunnels operating at very low densities were developed starting in about 1960.
低密度超音速风洞大约开始发展于1960年。