PHYSICAL MODEL OF THE SWEPT SHOCK-WAVE BOUNDARY-LAYER INTERACTION FLOWFIELD

被引:104
作者
ALVI, FS [1 ]
SETTLES, GS [1 ]
机构
[1] PENN STATE UNIV,GAS DYNAM LAB,UNIV PK,PA 16802
关键词
D O I
10.2514/3.11212
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
New data are presented on the structure of fin-induced, swept shock/boundary-layer interactions. These data are obtained using a nonintrusive planar laser scattering (PLS) imaging technique. A range of interaction strengths, from barely separated to very strongly separated, is covered for freestream Mach numbers of 3 and 4. These new data, when combined with previous results on the flowfield and interaction "footprint," are sufficient to allow the construction of a physical model for the swept interaction flowfield structure and behavior. This physical model is presented and discussed in terms of six detailed flowfield maps which take advantage of the inherent quasiconical behavior of the class of interactions considered.
引用
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页码:2252 / 2258
页数:7
相关论文
共 26 条
[1]  
ALVI FS, 1990, AIAA901644 PAP
[2]   2-WAVELENGTH LASER TRANSMISSOMETER FOR MEASUREMENTS OF THE MEAN SIZE AND CONCENTRATION OF COAL ASH DROPLETS IN COMBUSTION FLOWS [J].
ARIESSOHN, PC ;
SELF, SA ;
EUSTIS, RH .
APPLIED OPTICS, 1980, 19 (22) :3775-3781
[4]  
BOHREN CF, 1983, ABSORPTION SCATTERIN, pCH13
[5]  
BOHREN CF, 1990, COMMUNICATION AUG
[6]  
CLEMENS NT, 1991, EXP FLUIDS, V11, P175, DOI 10.1007/BF00190296
[7]  
DURBIN EJ, 1951, NACA TN2441
[8]  
GARG SS, 1990, UNPUB COMMUNICATION
[9]  
HORSTMAN CC, 1986, AIAA861032 PAP
[10]  
HSU JC, 1992, AIAA920746 PAP