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A Further Compilation of Compressible Boundary Layer Data with a Survey of Turbulence Data.


ADA111638

Publication Date 1981
Personal Author Fernholz, H. H.; Finley, P. J.; Mikulla, V.
Page Count 220
Abstract This volume is a continuation of AGARDographs 223.253 (Fernholz and Finley 1977, 1980). The data compilation for 59 nominally two dimensional compressible shock-free flows presented in AGARD0graph 223 is supplemented by a further 18 cases, including some shock-boundary-layer-interactions. The data are also available on magnetic tape from AGARD centres as for AGARD 223. The text preceding the compilation gives a review of the available turbulence measurements. The measurements are compared on the basis of inner and outer region similarity relationships. There is little evidence of any quantitative correlation between different experiments. There is also an examination of the breakdown conditions for the Van-Driest-Crocco meanflow temperature-velocity correlation and the associated transformation procedures. The effects of extreme transverse curvature on the mean flow are briefly considered.
Keywords
  • Turbulent boundary layer
  • Compressible flow
  • Turbulent flow
  • Two dimensional flow
  • Boundary layer flow
  • Experimental data
  • Pressure gradients
  • Reynolds number
  • Hot wire anemometers
  • Shear stresses
  • Transformations
  • Shock waves
  • Foreign technology
  • NATO furnished
  • Shock boundary layer interaction
Source Agency
  • Non Paid ADAS
NTIS Subject Category
  • 46B - Fluid Mechanics
  • 51A - Aerodynamics
Corporate Authors Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine (France).
Supplemental Notes Continuation of AD-A045 367 and AD-A087 704.
Document Type Technical Report
NTIS Issue Number 198213
A Further Compilation of Compressible Boundary Layer Data with a Survey of Turbulence Data.
A Further Compilation of Compressible Boundary Layer Data with a Survey of Turbulence Data.
ADA111638

  • Turbulent boundary layer
  • Compressible flow
  • Turbulent flow
  • Two dimensional flow
  • Boundary layer flow
  • Experimental data
  • Pressure gradients
  • Reynolds number
  • Hot wire anemometers
  • Shear stresses
  • Transformations
  • Shock waves
  • Foreign technology
  • NATO furnished
  • Shock boundary layer interaction
  • Non Paid ADAS
  • 46B - Fluid Mechanics
  • 51A - Aerodynamics
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