| | Prediction of Very High Reynolds Number Compressible Skin Friction, AIAA 98-2880, June 15-18, 1998, (Site not responding. Last check: 2007-11-07) |
 | | Abstract : Flat plate skin friction calculations over a range of Mach numbers from 0.4 to 3.5 at Reynolds numbers from 16 million to 492 million using a Navier Stokes method with advanced turbulence modeling are compared with incompressible skin friction coefficient correlations. |
 | | The semi-empirical correlation theories of van Driest; Cope; Winkler and Cha; and Sommer and Short T' are used to transform the predicted skin friction coefficients of solutions using two algebraic Reynolds stress turbulence models in the Navier-Stokes method PAB3D. |
 | | In general, the predicted skin friction coefficients scaled well with each reference temperature theory though, overall the theory by Sommer and Short appeared to best collapse the predicted coefficients. |
| techreports.larc.nasa.gov /ltrs/98/aiaa/NASA-aiaa-98-2880.refer.html (233 words) |