EFFECTS OF PRESSURE GRADIENTS ON TURBULENT-BOUNDARY-LAYER WALL-PRESSURE FLUCTUATIONS

被引:72
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SCHLOEMER, HH
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10.1121/1.1910581
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O42 [声学];
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070206 ; 082403 ;
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页码:93 / +
页数:1
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共 28 条
[1]  
BAKEWELL HP, 1962, USN559 UND SOUND LAB, P1
[2]  
BRADSHAW P, 1965, NPL1172 AER REPT, P1
[3]  
BULL MK, 1961, AASU199 U SOUTH REPT, P1
[4]  
BULL MK, 1963, AASU243 U SOUTH REP, P1
[5]   TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS [J].
CLAUSER, FH .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (02) :91-108
[6]   THE LAW OF THE WAKE IN THE TURBULENT BOUNDARY LAYER [J].
COLES, D .
JOURNAL OF FLUID MECHANICS, 1956, 1 (02) :191-226
[7]   THE STRUCTURE OF THE TURBULENT PRESSURE FIELD IN BOUNDARY-LAYER FLOWS [J].
CORCOS, GM .
JOURNAL OF FLUID MECHANICS, 1964, 18 (03) :353-378
[8]   RESOLUTION OF PRESSURE IN TURBULENCE [J].
CORCOS, GM .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1963, 35 (02) :192-&
[9]  
CORCOS GM, 1962, U CALIF I ENG RES SE, V183, P1
[10]  
GARDNER S, 1963, TRG142TN635 REPT, P1