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Numerical simulation of the hypersonic flow around lifting vehicles
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chaussee, Denny Rizk, Yehia Steger, Joseph |
| Copyright Year | 1987 |
| Description | A method for solving the viscous hypersonic flow field around realistic configurations is presented. The numerical procedure for generating the required finite difference grid and the two-factored implicit flow solver are described. Results are presented for the shuttle orbiter and a generic wing-body configuration at hypersonic Mach numbers. |
| File Size | 9228941 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870012683 |
| Archival Resource Key | ark:/13960/t3hx67d1m |
| Language | English |
| Publisher Date | 1987-04-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Body-wing Configurations Computational Fluid Dynamics Digital Simulation Hypersonic Flow Space Shuttle Orbiters Navier-stokes Equation Flow Equations Aerodynamic Configurations Finite Difference Theory Flow Distribution Flux Vector Splitting Computational Grids Viscous Flow Hyperbolic Differential Equations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |