基本释义:

亚音速风洞

网络释义

1)subsonic wind tunnel,亚音速风洞

2)supersonic wind tunnel,超音速风洞

3)trisonic tunnel,三音速风洞

4)transonic wind tunnel,跨音速风洞

5)subsonic wind tunnel,亚声速风洞

6)anechoic flow facility,消音风洞

用法和例句

Moiré) tomography is applied to measure the complex density distribution in supersonic wind tunnel.

使用叠栅层析技术解决超音速风洞中复杂密度场的测量难题。

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。

Although strain gage balances have been most useful in transonic and supersonic tunnels, they are by no means excluded from lowspeed work.

虽然，应变天平最适用于跨超音速风洞，但丝毫不意味着不能用于低速实验。

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

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)

The Test and Calibration of Φ200 Hypersonic Wind Tunnel

Φ200高超声速风洞调试和流场校测

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

Supersonic or ultrasonic meter

超音速（波）测速仪

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。

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

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

trisonic aerodynamics

三音速(亚音速、跨音速 、超音速)空气动力学

New Discovery on Karst Scenery Cave:Jiangyou Guanyin Cave

喀斯特风景溶洞的新发现:江油观音洞

a sonic boom follows an aircraft as a wake follows a ship.

超音速飞行会产生音爆。

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。

Research on Wind Speed Control System for Wind Tunnel Based on PLC;

基于PLC的风洞风速调控系统的研究

transsuper aerodynamics

跨音速和超音速空气动力学

This paper describes the investigation of boundary layer separation control for supercritical aerofoil using micro vortex generator in the low speed wind tunnel.

在低速风洞中研究了微型涡流发生器对超临界翼型边界层分离的控制。

hypersonic manned aircraft

高超音速有人驾驶飞机