Multiscale Reduced-Order Modeling of a Titanium Skin Panel Subjected to Thermomechanical Loading
Author:
Affiliation:
1. University of Wyoming, Laramie, Wyoming 82071
2. Imperial College London, London, England SW72AZ, United Kingdom
3. Vanderbilt University, Nashville, Tennessee 37240
Funder
University of Wyoming Faculty Start-Up Funding
Air Force Office of Science Research Multi-Scale Structural Mechanics and Prognosis Program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060497
Reference82 articles.
1. Characterization of Structural Response to Hypersonic Boundary-Layer Transition
2. Assessing Hypersonic Boundary-Layer Stability in the Presence of Structural Deformation
3. Interplay of Surface Deformation and Shock-Induced Separation in Shock/Boundary-Layer Interactions
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