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Numerical computation of viscous blunt body flows with a planar impinging shock
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tannehill, J. C. Rakich, J. V. Holst, T. L. |
| Copyright Year | 1974 |
| Description | Two- and three-dimensional, viscous blunt body flows with planar impinging shocks are computed using an explicit, time-dependent, finite-difference method to solve the complete set of Navier-Stokes equations. The bow shock is treated as a discontinuity, while all interior shock layer detail such as shear layers, shock waves, jets and the wall boundary layer are automatically captured in the solution. Numerical results are presented for cases in which planar shock waves of different strengths and orientations are allowed to impinge on the flow field surroundings an infinite cylinder resulting in two- and three-dimensional shock interference patterns. The numerical results are compared with experiment. |
| File Size | 604738 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010439 |
| Archival Resource Key | ark:/13960/t7kq2s78h |
| Language | English |
| Publisher Date | 1974-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Shock Waves Flow Equations Numerical Analysis Finite Difference Theory Flow Visualization Flow Characteristics Blunt Bodies Viscous Flow Boundary Layer Flow 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 |