| タイトル | Navier-Stokes simulation of 3-D hypersonic equilibrium air flow |
| 著者（英） | Nagaraj, N.; Lombard, C. K.; Bardina, J. |
| 著者所属（英） | PEDA Corp. |
| 発行日 | 1988-06-01 |
| 言語 | eng |
| 内容記述 | A computationally efficient three-dimensional conservative supracharacteristic Navier-Stokes method has been extended to simulate complex external chemically reacting flows of hypersonic reentry vehicles at angle-of-attack. Numerical simulation results of the flow around a sphere-cone-cone-flare reentry vehicle at 10 deg angle-of-attack are presented, in addition to the results of a well-validated two-dimensional code with which the 0-deg axisymmetric flow has been computed. A method for obtaining compositions of species in equilibrium ionized air is proposed. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 88A43751
AIAA PAPER 88-2695 |
| 権利 | Copyright |
