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Hypersonic flow analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chow, Chuen-Yen Ryan, James S. |
| Copyright Year | 1987 |
| Description | While the zonal grid system of Transonic Navier-Stokes (TNS) provides excellent modeling of complex geometries, improved shock capturing, and a higher Mach number range will be required if flows about hypersonic aircraft are to be modeled accurately. A computational fluid dynamics (CFD) code, the Compressible Navier-Stokes (CNS), is under development to combine the required high Mach number capability with the existing TNS geometry capability. One of several candidate flow solvers for inclusion in the CNS is that of F3D. This upwinding flow solver promises improved shock capturing, and more accurate hypersonic solutions overall, compared to the solver currently used in TNS. |
| File Size | 1308597 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870018213 |
| Archival Resource Key | ark:/13960/t0cv9d70b |
| Language | English |
| Publisher Date | 1987-08-31 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Geometry Boundary Value Problems Computational Fluid Dynamics Interactional Aerodynamics Flow Distribution Hypersonic Flow Computational Grids Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |