| タイトル | The NASA High Speed ASE Project: Computational Analyses of a Low-Boom Supersonic Configuration |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140011900 |
| 著者（英） | Christhilf, David M.; Johnson, Christopher; Kopasakis, George; Bounajem, Elias G.; Yoo, Seung Y.; DeLaGarza, Antonio; Zink, Scott; Sanetrik, Mark D.; Buonanno, Michael; Chwalowski, Pawel; Silva, Walter A. |
| 発行日 | 2014-01-13 |
| 言語 | eng |
| 内容記述 | A summary of NASA's High Speed Aeroservoelasticity (ASE) project is provided with a focus on a low-boom supersonic configuration developed by Lockheed-Martin and referred to as the N+2 configuration. The summary includes details of the computational models developed to date including a linear finite element model (FEM), linear unsteady aerodynamic models, structured and unstructured CFD grids, and discussion of the FEM development including sizing and structural constraints applied to the N+2 configuration. Linear results obtained to date include linear mode shapes and linear flutter boundaries. In addition to the tasks associated with the N+2 configuration, a summary of the work involving the development of AeroPropulsoServoElasticity (APSE) models is also discussed. |
| NASA分類 | Aerodynamics |
| レポートNO | AIAA Paper 2014-0675
NF1676L-16637 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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