Modeling Hypersonic Propulsion Using Finite Element CFD-Reference-Cited by-同舟云学术

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Modeling Hypersonic Propulsion Using Finite Element CFD

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Moffitt Nicholas¹,Pinkerman Cody¹,Arena Andrew¹

Affiliation:

1. Oklahoma State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-400

Reference12 articles.

1. Current grid-generation strategies and future requirements in hypersonic vehicle design, analysis and testing

2. 3Cowan, T. "Finite Element CFD Analysis of Super-Maneuvering and Spinning Structures," Ph.D. Dissertation,Oklahoma StateUniversity,2003.

3. 4Gupta,K.K.,Meek,J.L.,FiniteElementMultidisciplinaryAnalysis,AIAAEducationalSeries,AIAA,Reston,VA,2000.

4. Aircraft Flight Dynamics with a Non-Inertial CFD Code

Cited by 2 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. Comparison of Methods for Implementing Well-Posed Boundary Conditions in Galerkin CFD Solvers;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

2. Propulsion Models Implemented in Finite Element CFD;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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