| タイトル | Application of Adjoint Methodology in Various Aspects of Sonic Boom Design |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011457 |
| 著者（英） | Rallabhandi, Sriram K. |
| 発行日 | 2014-06-16 |
| 言語 | eng |
| 内容記述 | One of the advances in computational design has been the development of adjoint methods allowing efficient calculation of sensitivities in gradient-based shape optimization. This paper discusses two new applications of adjoint methodology that have been developed to aid in sonic boom mitigation exercises. In the first, equivalent area targets are generated using adjoint sensitivities of selected boom metrics. These targets may then be used to drive the vehicle shape during optimization. The second application is the computation of adjoint sensitivities of boom metrics on the ground with respect to parameters such as flight conditions, propagation sampling rate, and selected inputs to the propagation algorithms. These sensitivities enable the designer to make more informed selections of flight conditions at which the chosen cost functionals are less sensitive. |
| NASA分類 | Aircraft Design, Testing and Performance; Aerodynamics |
| レポートNO | NF1676L-18886
AIAA Paper 2014-2271 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
