Integrated Aerothermoelastic Analysis Framework with Application to Skin Panels-Reference-Cited by-同舟云学术

Integrated Aerothermoelastic Analysis Framework with Application to Skin Panels

Published:2018-11 Issue:11 Volume:56 Page:4562-4581
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Huang Daning¹,Rokita Tomer¹,Friedmann Peretz P.¹

Affiliation:

1. University of Michigan, Ann Arbor, Michigan 48109

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056677

Reference45 articles.

1. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future

2. McNamaraJ. J. “Aeroelastic and Aerothermoelastic Behavior of Two and Three Dimensional Lifting Surfaces in Hypersonic Flow,” Ph.D. Thesis, Univ. of Michigan, Ann Arbor, MI, 2005.

3. LamorteN. E. “Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis,” Ph.D. Thesis, Univ. of Michigan, Ann Arbor, MI, 2013.

4. Partitioned analysis of coupled mechanical systems

5. Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity

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