| contributor author | L. T. Chen | |
| contributor author | D. A. Caughey | |
| date accessioned | 2017-05-08T23:09:02Z | |
| date available | 2017-05-08T23:09:02Z | |
| date copyright | September, 1980 | |
| date issued | 1980 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26962#309_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93461 | |
| description abstract | Finite difference solutions for transonic flowfields about engine inlet nacelles are obtained by combining a general grid-generation scheme with a previously developed general solver for transonic potential flowfields (1). The grid-generation scheme is similar to Thompson’s method, but uses simpler equations to solve for the mesh coordinates. An extrapolated relaxation procedure is used to obtain improved convergence of the transonic solution to small residuals. Results obtained for flowfields with embedded supersonic regions both outside and inside the inlets compare well with experimental results. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Transonic Inlet Flow Calculations Using a General Grid-Generation Scheme | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3240687 | |
| journal fristpage | 309 | |
| journal lastpage | 315 | |
| identifier eissn | 1528-901X | |
| keywords | Flow (Dynamics) | |
| keywords | Mesh generation | |
| keywords | Engines | |
| keywords | Relaxation (Physics) AND Equations | |
| tree | Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 003 | |
| contenttype | Fulltext | |