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.
引用
收藏
页码:1 / 57
页数:57
相关论文
共 164 条
[61]  
HOPKINS EJ, 1966, D3478 NASA TN
[62]  
HSU EY, 1955, 957 D TAYL MOD BAS R
[63]   A TRANSFORMATION FOR COMPRESSIBLE TURBULENT BOUNDARY LAYERS WITH AIR INJECTION [J].
JEROMIN, LOF .
JOURNAL OF FLUID MECHANICS, 1968, 31 :65-&
[64]  
JOHNSTON JP, 1960, J BAS ENG ASME, V82
[65]  
Keener E.R., 1969, D5544 NASA TN
[66]  
KEENER ER, AIAA69345 PAP
[67]  
KEMPF G, 1929, WERFT REEDEREI HAFEN, P234
[68]  
Klein E. J., 1970, Review of Scientific Instruments, V41, P238, DOI 10.1063/1.1684477
[69]  
KLEIN EJ, 1969, X1774 NASA TM
[70]  
KLEIN EJ, 1968, P COMPUTATION TURBUL