OUTLINE OF TECHNIQUES AVAILABLE FOR MEASUREMENT OF SKIN FRICTION IN TURBULENT BOUNDARY-LAYERS

被引:163
作者
WINTER, KG [1 ]
机构
[1] ROYAL AIRCRAFT ESTAB,FARNBOROUGH GU14 6TD,HAMPSHIRE,ENGLAND
关键词
D O I
10.1016/0376-0421(77)90002-1
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The techniques covered include force-measurement balances, the use of the velocity profile, pressure measurements by surface pitot tubes or about obstacles, and the use of the analogies of heat transfer, mass transfer or surface oil-flow. Hot-wire or laser techniques for determining the shear stress within the fluid are not included. The sources of error and ranges of application of the various techniques are discussed. © 1979.
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页码:1 / 57
页数:57
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共 164 条
[1]  
ALLEN JM, 1973, D7190 NASA TN
[2]  
Allen JM, 1976, D8291 NASA TN
[3]  
ALLEN JM, 1968, D4853 NASA TN
[4]   VELOCITY PROFILES IN TURBULENT COMPRESSIBLE BOUNDARY LAYERS [J].
BARONTI, PO ;
LIBBY, PA .
AIAA JOURNAL, 1966, 4 (02) :193-&
[5]   DETERMINATION OF MEAN AND DYNAMIC SKIN FRICTION SEPARATION AND TRANSITION IN LOW-SPEED FLOW WITH A THIN-FILM HEATED ELEMENT [J].
BELLHOUSE, BJ ;
SCHULTZ, DL .
JOURNAL OF FLUID MECHANICS, 1966, 24 :379-+
[6]   MEASUREMENT OF FLUCTUATING SKIN FRICTION IN AIR WITH HEATED THIN-FILM GAUGES [J].
BELLHOUSE, BJ ;
SCHULTZ, DL .
JOURNAL OF FLUID MECHANICS, 1968, 32 :675-+
[7]  
BELLHOUSE BT, 1965, RM3490 ARC
[8]  
BERTELRUD A, 1976, AU1133 FFA TECHN NOT
[9]   EVALUATION OF PRESTON TUBE CALIBRATION EQUATIONS IN SUPERSONIC-FLOW - COMMENT [J].
BRADSHAW, P ;
UNSWORTH, K .
AIAA JOURNAL, 1974, 12 (09) :1293-1295
[10]   A SIMPLE METHOD FOR DETERMINING TURBULENT SKIN FRICTION FROM VELOCITY PROFILES [J].
BRADSHAW, P .
JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (12) :841-841