Development of a Defect Stream Function, Law of the Wall/wake Method for Compressible Turbulent Boundary LayersNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Compressibility - 114 pages |
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accuracy accurate agreement AIAA allows analytic analytic solution application approach approximately baseline boundary condition Clauser coefficient compares comparison completely compressible computed constant constrained zero-order coordinate corresponding defect stream function defined density derivation determined developed difference discussed eddy eddy-viscosity model edge Effect empirical equilibrium flow existing experiment experimental data expressions Figure flat plate flowfield Fluid formulation full eqns given governing equation grid point implementation incompressible flow increases inner region integral Journal limit logarithmic match point mean Mellor and Gibson normal Note numerical numerical computations obtained outer region parameter patch physically present method pressure gradient procedure range reduces reference relationship respectively result shear shear-stress velocity ratio shown shows slip-velocity solutions streamwise stress surface technique term transformation turbulence model turbulent boundary layers valid values variable various velocity defect profiles velocity profiles viscosity wake wall