Development of an efficient inverse method for supersonic and hypersonic body design
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26452
Reference19 articles.
1. The design of transonic aerofoils by a well-posed inverse method
2. The role of constraints in the inverse design problem for transonic airfoils
Cited by 3 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. Inverse Solution Uniqueness and Domain of Existence for Space-Marching Applications;AIAA Journal;2000-01
2. A viscous inverse method for the high speed axisymmetric body design;7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;1998-08-22
3. New Three-Dimensional Inverse Method for High-Speed Vehicle Design;Journal of Spacecraft and Rockets;1998-07
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