An Overview of the NASA High Speed ASE Project: Aeroelastic Analyses of a Low-Boom Supersonic Configuration
Author:
Affiliation:
1. NASA Langley Research Center
2. Lockheed Martin Corporation
3. NASA Armstrong Flight Research Center
4. NASA Glenn Research Center
5. Analytical Mechanics Associates, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0684
Reference21 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Aero-Propulso-Elastic Analysis of a Supersonic Transport;Journal of Aircraft;2020-07
2. Parametric Fluid-structural Interaction Reduced Order Models in Continuous Time Domain for Aeroelastic Analysis of High-speed Vehicles;AIAA Scitech 2020 Forum;2020-01-05
3. Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration;33rd AIAA Applied Aerodynamics Conference;2015-06-19
4. Ongoing Fixed Wing Research within the NASA Langley Aeroelasticity Branch;33rd AIAA Applied Aerodynamics Conference;2015-06-19
5. Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints;33rd AIAA Applied Aerodynamics Conference;2015-06-19
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