Global Surface Pressure Pattern for a Compressible Elliptical Cavity Flow Using Pressure-Sensitive Paint

被引:1
作者
Huang, Yi-Xuan [1 ]
Chung, Kung-Ming [2 ]
机构
[1] Natl Cheng Kung Univ, Dept Aeronaut & Astronaut, Tainan 701, Taiwan
[2] Natl Cheng Kung Univ, Aerosp Sci & Technol Res Ctr, Tainan 711, Taiwan
关键词
elliptical cavity; eccentricity; pressure-sensitive paint; high subsonic flow;
D O I
10.3390/aerospace11020159
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The flow field in a cavity depends on the properties of the upstream boundary layer and the cavity geometry. Comprehensive studies for rectangular cavities have been conducted. This experimental study determines the global surface pressure pattern for elliptical cavities (eccentricities of 0, 0.66 and 0.87) in a naturally developed turbulent boundary layer using pressure-sensitive paint. The ratio between the length (major axis) and the depth is 4.43-21.5, and the freestream Mach number is 0.83. The mean surface pressure distribution of an elliptical cavity resembles that of a rectangular cavity. A change in the value of eccentricity (wall curvature) affects the region for an adverse pressure gradient in an open cavity, an extension of the plateau in a transitional-closed cavity and flow expansion near the front and rear edges. The boundaries between an open, transitional and closed cavities vary.
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页数:12
相关论文
共 23 条
[1]   Surface pressure measurements using luminescent coatings [J].
Bell, JH ;
Schairer, ET ;
Hand, LA ;
Mehta, RD .
ANNUAL REVIEW OF FLUID MECHANICS, 2001, 33 :155-206
[2]   AN INVESTIGATION OF SEPARATED FLOWS .1. THE PRESSURE FIELD [J].
CHARWAT, AF ;
ROOS, JN ;
DEWEY, FC ;
HITZ, JA .
JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (06) :457-470
[3]   Reynolds number dependence of flow past a shallow open cavity [J].
Chen Huai ;
Zhong Qiang ;
Wang XingKui ;
Li DanXun .
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2014, 57 (11) :2161-2171
[4]   Characteristics of transonic rectangular cavity flows [J].
Chung, KM .
JOURNAL OF AIRCRAFT, 2000, 37 (03) :463-468
[5]   Three-dimensional effect on transonic rectangular cavity flows [J].
Chung, KM .
EXPERIMENTS IN FLUIDS, 2001, 30 (05) :531-536
[6]   Reynolds number effect on compressible cylindrical cavity flow [J].
Chung, Kung-Ming ;
Huang, Yi-Xuan ;
Lee, Kuan-Huang ;
Chang, Keh-Chin .
CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (02) :456-464
[7]   Characteristics of cylindrical cavities in a compressible turbulent flow [J].
Chung, Kung-Ming ;
Lee, Kuan-Huang ;
Chang, Keh-Chin .
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 66 :160-164
[8]   On aerodynamic characteristics of rarefied hypersonic flows over variable eccentricity elliptical cavities [J].
Guo, Guangming ;
Luo, Qin ;
Wu, Jinwu .
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 134
[9]  
Heller HE, 1975, Air Force Flight Dynamics Laboratory Technical Report No. AFFDL-TR-74-133
[10]   Flow regimes and drag characteristics of yawed elliptical cavities with varying depth [J].
Hering, Thomas ;
Savory, Eric .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2007, 129 (12) :1577-1583