1) wind tunnel free-flight
风洞自由飞
2) wind tunnel free flight experiment
风洞自由飞实验
1.
Our wind tunnel free flight experiment results show that this kind of shape when M=5 generates conical destabilization,and its occurrence rate reaches 100%.
但是简单尖锥体、小钝锥体我们的风洞自由飞实验结果(M=5):会产生锥动失稳,甚至实验次数中出现锥动失稳的比例达100%。
3) free jet tunnel
自由射流风洞
1.
, on the performances of the submerged inlet are investigated experimentally in a low speed free jet tunnel with a Mach number of 0.
1自由射流风洞上 ,对影响出口流场畸变的埋入式进气道的唇口、内通道形状等因素进行了实验研究 。
4) free jet wind tunnel
自由喷射风洞
5) free jet wind tunnel
自由射流式风洞
6) free-piston shock tunnel
自由活塞激波风洞
1.
The numerical method is a development from the operating principle of a heavy piston compressor and the utility program is very important to the design and calibration of a free-piston shock tunnel.
该方法是对自由活塞激波风洞运行理论的发展，形成的计算软件可直接应用于自由活塞激波风洞的设计和状态调试。
补充资料：必然王国与自由王国(见必然与自由)
必然王国与自由王国(见必然与自由)
realm of necessity and realm of freedom
of口1 Iun Wongg口0 yU ZlyQU wangguo必然王国与自由王国(realmandrealm of freedom)necessity见必然与自由。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条