| タイトル | A performance index approach to aerodynamic design with the use of analysis codes only |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880009168 |
| 著者（英） | Moitra, Anutosh; Barger, Raymond L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1988-03-01 |
| 言語 | eng |
| 内容記述 | A method is described for designing an aerodynamic configuration for a specified performance vector, based on results from several similar, but not identical, trial configurations, each defined by a geometry parameter vector. The theory shows the method effective provided that: (1) the results for the trial configuration provide sufficient variation so that a linear combination of them approximates the specified performance; and (2) the difference between the performance vectors (including the specifed performance) are sufficiently small that the linearity assumption of sensitivity analysis applies to the differences. A computed example describes the design of a high supersonic Mach number missile wing body configuration based on results from a set of four trial configurations. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88N18552
L-16379
NAS 1.60:2805
NASA-TP-2805 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/147053 |
