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Measurements of Fluctuating Pressures in 8- BY 6-Foot Supersonic Wind Tunnel for Mach Number Range of 0.56 to 2.07

机译：测量8-BY 6英尺超音速风洞中的脉动压力，马赫数范围为0.56至2.07

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作者
Karabinus, R. J.; Sanders, B. W.;
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年度 1970
页码 1-3
总页数 3
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Pressure measurements ; Pressure oscillations ; Supersonic wind tunnels ; Background noise ; Graphs (charts) ; Oscillographs ; Porous walls ; Pressure sensors ; Transonic compressors;

机译：压力测量;压力振荡;超音速风洞;背景噪声;图形（图表）;示波器;多孔壁;压力传感器;跨音速压缩机;

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机译：受强大背景噪声影响的风洞数据下湍流边界层压力波动的相位速度
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3. Fluctuating and mean pressure measurements on a stadium covering in wind tunnel [J] . J. Marighetti, A. Wittwer, M. De Bortoli, Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2000,第3期

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5. Hypersonic wind-tunnel measurements of boundary-layer pressure fluctuations. [D] . Casper, Katya M. 2009

机译：边界层压力波动的高超音速风洞测量。
6. Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel [O] . M. Anyoji, D. Numata, H. Nagai, -1

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7. Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel [O] . Pickett, Mark T., Arrington, E. Allen 1992

机译：NASA Lewis研究中心8英尺6英尺超音速/ 9英尺15英尺低速风洞的流动质量研究
8. Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 [R] . Karabinus, R. J., Sanders, B. W. 1970

机译：测量8×6英尺超音速风洞的波动压力，马赫数范围为0.56至2.07

Measurements of Fluctuating Pressures in 8- BY 6-Foot Supersonic Wind Tunnel for Mach Number Range of 0.56 to 2.07

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