SOME WIND-TUNNEL TEST DEVELOPMENTS RELATING TO FLUCTUATING PRESSURES OF TRANSONIC SHOCK-BOUNDARY LAYER INTERACTION

被引：0
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作者：
LUKSUS, EJ
HUANG, JT
机构：
来源：
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA | 1970年 / 47卷 / 1P1期
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D O I：
10.1121/1.1974645
中图分类号：
O42 [声学];
学科分类号：
070206 ; 082403 ;
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页码：63 / &
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