SIMPLE SUPERSONIC WIND-TUNNEL

被引：0
|
作者：
BYKOV, DF
GRITSININ, SI
RAEVSKII, IM
机构：
来源：
INSTRUMENTS AND EXPERIMENTAL TECHNIQUES | 1991年 / 34卷 / 02期
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D O I：
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中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The switching element of the wind tunnel is a stock KMU-25 valve with slight modifications. Supersonic gas flows with a static pressure of 150 torr are produced; the gas-jet diameter is 4 cm; the duration of the quasistationary escape stage is approximately 50 msec; and the Mach number is approximately 3.
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页码：445 / 446
页数：2
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