Flutter and Limit Cycle Oscillations of Cantilevered Plate in Supersonic Flow
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
DOD Smart Scholarship for Service
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035992
Reference32 articles.
1. Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions
2. A theoretical computational model of a plate in hypersonic flow
3. Hypersonic Fluid–Structure Interaction on a Cantilevered Plate with Shock Impingement
4. Nonlinear Structural Mechanics
5. Refined models of elastic beams undergoing large in-plane motions: Theory and experiment
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