FAR WAKE BEHIND CYLINDERS AT HYPERSONIC SPEEDS .I. FLOWFIELD

被引:16
作者
BEHRENS, W
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D O I
10.2514/3.4398
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V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:2135 / &
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[1]   VISCOUS INTERACTION EFFECTS ON A STATIC PRESSURE PROBE AT M=6 [J].
BEHRENS, W .
AIAA JOURNAL, 1963, 1 (12) :2864-2866
[2]  
BEHRENS W, 1966, THESIS CALIFORNIA I
[3]   MEASURED TRANSITION FROM LAMINAR TO TURBULENT FLOW AND SUBSEQUENT GROWTH OF TURBULENT WAKES [J].
CLAY, WG ;
LABITT, M ;
SLATTERY, RE .
AIAA JOURNAL, 1965, 3 (05) :837-&
[4]   NEAR WAKE OF A BLUNT BODY AT HYPERSONIC SPEEDS [J].
DEWEY, CF .
AIAA JOURNAL, 1965, 3 (06) :1001-&
[5]   HOT WIRE MEASUREMENTS IN LOW REYNOLDS NUMBER HYPERSONIC FLOWS [J].
DEWEY, CF .
ARS JOURNAL, 1961, 31 (12) :1709-1718
[6]  
DEWEY CF, 1963, THESIS CALIFORNIA I
[7]   ON TRAILS OF AXISYMMETRIC HYPERSONIC BLUNT BODIES FLYING THROUGH THE ATMOSPHERE [J].
FELDMAN, S .
JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (06) :433-&
[8]  
FELDMAN S, 1959, 82 AVC RES REPT
[9]   LAMINAR WAKE WITH ARBITRARY INITIAL PROFILES [J].
GOLD, H .
AIAA JOURNAL, 1964, 2 (05) :948-949
[10]  
HAYES WD, 1959, HYPERSONIC FLOW THEO, pCH9