NASA NTRS ยท 19820036248
Turbulence modeling for computational aerodynamics
Abstract
The status of turbulence modeling for external aerodynamic flows is reviewed, and closure concepts for the compressible form of the Reynolds-averaged Navier-Stokes equations are briefly outlined to establish a framework for comparison. The importance of experimental requirements for developing and verifying turbulence models is emphasized. Attention is then given to three important flow categories: attached flows, separating and reattaching flows, and trailing-edge flows. Examples of comparisons between experiments and computations for twoand three-dimensional flows are presented to illustrate the status of modeling. It is shown that, for most two-dimensional attached flows, eddy viscosity concepts will probably be adequate. For attached three-dimensional flows, however, eddy-viscosity and Reynolds-stress models are both deficient, failing to predict the proper surface shear-stress in rapidly skewing boundary layers, regardless of whether they are pressure driven or strain driven.
Keep this discovery
Explore connections, maps & timelines
Marvin, J. G.. 1982-01-01. Turbulence modeling for computational aerodynamics. https://ntrs.nasa.gov/citations/19820036248
Cite the original work for its findings. Save a collection to share your selection of sources.