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Viscous-shock-layer analysis of hypersonic flows over long slender vehicles. ph.d. thesis, 1988
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lee, Kam-Pui Gupta, Roop N. |
| Copyright Year | 1992 |
| Description | An efficient and accurate method for solving the viscous shock layer equations for hypersonic flows over long slender bodies is presented. The two first order equations, continuity and normal momentum, are solved simultaneously as a coupled set. The flow conditions included are from high Reynolds numbers at low altitudes to low Reynolds numbers at high altitudes. For high Reynolds number flows, both chemical nonequilibrium and perfect gas cases are analyzed with surface catalytic effects and different turbulence models, respectively. At low Reynolds number flow conditions, corrected slip models are implemented with perfect gas case. Detailed comparisons are included with other predictions and experimental data. |
| File Size | 4995135 |
| Page Count | 226 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920014300 |
| Archival Resource Key | ark:/13960/t2b905v4r |
| Language | English |
| Publisher Date | 1992-03-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer High Reynolds Number Low Reynolds Number Hypersonic Flow Momentum Shock Layers Chemical Equilibrium Low Altitude Turbulence Models Flow Distribution Ideal Gas Catalysis Slender Bodies Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Thesis |
