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Numerical study of unsteady viscous hypersonic blunt body flows with an impinging shock
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Yee, H. C. Klopfer, G. H. Kutler, P. |
| Copyright Year | 1988 |
| Description | A complex two-dimensional, unsteady, viscous hypersonic shock wave interaction is numerically simulated by a high-resolution, second-order fully implicit shock-capturing scheme. The physical model consists of a nonstationary oblique shock impinging on the bow shock of a blunt body. Studies indicated that the unsteady flow patterns are slightly different from their steady counterparts. However, for the sample cases investigated the peak surface pressures for the unsteady flows seem to occur at very different impingement locations than for the steady flow cases. |
| File Size | 473468 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19880013266 |
| Archival Resource Key | ark:/13960/t1jh8fn42 |
| Language | English |
| Publisher Date | 1988-04-01 |
| Access Restriction | Open |
| Subject Keyword | Numerical Analysis Navier-stokes Equation Hypersonic Speed Algorithms Computational Fluid Dynamics Bow Waves Flow Distribution Shock Wave Interaction Blunt Bodies Unsteady Flow Two Dimensional Flow Viscous 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 |