A Hypersonic Vehicle Model Generator for MASIV
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4563
Reference24 articles.
1. Proper Orthogonal Decomposition for Reduced-Order Thermal Solution in Hypersonic Aerothermoelastic Simulations
2. Modeling and Analysis Framework for Early Stage Trade-off Studies for Scramjet-Powered Hypersonic Vehicles
Cited by 6 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. Aeroelastic Control-Oriented Modeling of an Airbreathing Hypersonic Vehicle;Journal of Guidance, Control, and Dynamics;2018-05
2. A Brief Survey on Six-Degree-of-Freedom Modeling for Air-breathing Hypersonic Vehicles ⁎ ⁎This research was funded by the Air Force Research Laboratory through its Asian Office of Aerospace Research and Development (AOARD) under the contract number FA2386-15-1-14045.;IFAC-PapersOnLine;2018
3. Aeroelastic Control-oriented Modeling of an Air-breathing Hypersonic Vehicle;15th Dynamics Specialists Conference;2016-01-01
4. Minimum-Fuel Ascent of a Hypersonic Vehicle Using Surrogate Optimization;Journal of Aircraft;2014-11
5. Design Optimization of a Scramjet Vehicle for Ascent Using Surrogate Optimization;52nd Aerospace Sciences Meeting;2014-01-10
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