NASA-TP-1619
Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T18:28:55Z | |
| date available | 2017-09-04T18:28:55Z | |
| date copyright | 01/01/1980 | |
| date issued | 1980 | |
| identifier other | IRYKAEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/211072 | |
| description abstract | A numerically generated orthogonal coordinate system (with the body surface and shock wave as opposite boundaries) was applied with a time asymptotic method to obtain steady flow solutions for axisymmetric inviscid flow over several blunt bodies including spheres, paraboloids, ellipsoids, hyperboloids, hemisphere cylinders, spherically blunted cones, and a body with a concavity in the stagnation region. Comparisons with experimental data and with the results of other computational methods are discussed. The numerically generated orthogonal coordinate system is described and applications of the method to complex body shapes, particularly those with concave regions, are discussed. | |
| language | English | |
| title | NASA-TP-1619 | num |
| title | Application of a numerically generated orthogonal coordinate system to the solution of inviscid axisymmetric supersonic flow over blunt bodies | en |
| type | standard | |
| page | 62 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1980 | |
| contenttype | fulltext | |
| subject keywords | BLUNT | |
| subject keywords | BODIES | |
| subject keywords | BOUNDARY | |
| subject keywords | COORDINATES | |
| subject keywords | DISTRIBUTION | |
| subject keywords | FLOW | |
| subject keywords | GENERATION | |
| subject keywords | GRID | |
| subject keywords | INVISCID | |
| subject keywords | MATHEMATICS | |
| subject keywords | ORTHOGONALITY | |
| subject keywords | PROBLEMS | |
| subject keywords | SHOCK | |
| subject keywords | STEADY | |
| subject keywords | SUPERSONIC | |
| subject keywords | VALUE | |
| subject keywords | WAVES |

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