攻角动态变化对侧压式进气道起动特性影响的风洞试验
Wind tunnel experiment of the influence of dynamic change of attack angle on start property of sidewall compression scramjet inlet
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摘要: 为了探寻不同频率下攻角动态变化对进气道起动性能的影响,进行了攻角以不同频率调节的侧压式进气道Ma=3.85的风洞试验.对一个设计Ma=6、起动Ma=2.5的侧压式进气道完成了攻角从0°→8.15°→0°,频率分别为0.8,1.6,3.2 Hz和6 Hz的数次吹风试验.试验结果表明:四种频率状态下进气道在一个振荡周期中都能经历一个起动—不起动—再起动的过程;随着频率的增加,在进入振荡的第1个周期内不起动攻角缓慢增大,而在之后的周期性变化中不起动攻角急剧减小.Abstract: In order to explore how the change of attack angle at different frequencies influences the start property of inlet,this paper conducted a wind tunnel experiment for the sidewall compression scramjet inlet with Mach number 3.85 and attack angle at different frequencies.The sidewall compression scramjet inlet,with designed Mach number 6 and start Mach number 2.5,was subject to several flow tests,when attack angle changed from 0°to 8.15° again down to 0°,with the frequency at 0.8,1.6,3.2 Hz and 6 Hz,respectively.Results show that at each frequency,the inlet in a periodic oscillation succeeds to go through a start-unstart-restart process.With the increase of frequency,attack angle gradually goes up in the first periodic oscillation,and sharply goes down in the proceeding periodic oscillation.
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