| タイトル | Extended Conformal Mappings for Supersonic Aircraft Calculations |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760012986 |
| 著者（英） | Moretti, G. |
| 著者所属（英） | Polytechnic Inst. of New York |
| 発行日 | 1976-03-01 |
| 言語 | eng |
| 内容記述 | A gasdynamical analysis is presented for a three-dimensional, supersonic, inviscid, steady, shockless flow past an arbitrary airframe, using computational grids. The analysis, which includes special treatments for body points and bow-shock points, relies on the equations of motion written in terms of logarithm of pressure entropy and two angles reprising the velocity vector. A FORTRAN code was employed (sample geometry is shown). The flow analysis is considered reliable for aircraft cross-sections that are elliptical in shape. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 76N20074
NASA-CR-146541 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186611 |
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