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Near-wall modeling of compressible turbulent flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | So, Ronald M. C. |
| Copyright Year | 1991 |
| Description | A near-wall two-equation model for compressible flows is proposed. The model is formulated by relaxing the assumption of dynamic field similarity between compressible and incompressible flows. A postulate is made to justify the extension of incompressible models to ammount for compressibility effects. This requires formulation the turbulent kinetic energy equation in a form similar to its incompressible counterpart. As a result, the compressible dissipation function has to be split into a solenoidal part, which is not sensitive to changes of compressibility indicators, and a dilatational part, which is directly affected by these changes. A model with an explicit dependence on the turbulent Mach number is proposed for the dilatational dissipation rate. |
| File Size | 1952829 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910016051 |
| Archival Resource Key | ark:/13960/t1ck39n73 |
| Language | English |
| Publisher Date | 1991-06-30 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Turbulent Flow Compressibility Turbulent Boundary Layer Boundary Conditions Flow Equations Prandtl Number Compressibility Effects Energy Dissipation Flow Distribution Wall Flow Mathematical Models Kinetic Energy Compressible Flow Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |