Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies (Q1905642)
From MaRDI portal
| This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies |
scientific article; zbMATH DE number 832028
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies |
scientific article; zbMATH DE number 832028 |
Statements
Supersonic, turbulent flow computation and drag optimization for axisymmetric afterbodies (English)
0 references
3 June 1996
0 references
The compressible, turbulent flow about an axisymmetric body was numerically studied using the MacCormack unsplit explicit algorithm applied to the mass-average Navier-Stokes equations solved in conjunction with the \(k-\varepsilon\) turbulence model. Numerical predictions of total body drag (pressure drag, skin friction drag, and base drag) were made for an axisymmetric body six diameters in length, with and without a boattail. The golden section optimization method was used to optimize the body boattail angle for minimum drag.
0 references
\(k\)-epsilon turbulence model
0 references
MacCormack unsplit explicit algorithm
0 references
mass-average Navier-Stokes equations
0 references
golden section optimization method
0 references
body boattail angle
0 references
0 references