| タイトル | Boom Minimization Framework for Supersonic Aircraft Using CFD Analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100002817 |
| 著者（英） | Ordaz, Irian; Rallabhandi, Sriram K. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2010-01-04 |
| 言語 | eng |
| 内容記述 | A new framework is presented for shape optimization using analytical shape functions and high-fidelity computational fluid dynamics (CFD) via Cart3D. The focus of the paper is the system-level integration of several key enabling analysis tools and automation methods to perform shape optimization and reduce sonic boom footprint. A boom mitigation case study subject to performance, stability and geometrical requirements is presented to demonstrate a subset of the capabilities of the framework. Lastly, a design space exploration is carried out to assess the key parameters and constraints driving the design. |
| NASA分類 | Aerodynamics |
| レポートNO | LF99-8940
AIAA Paper 2010-1506 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
