Effects of Strain Hardening on Response of Skin Panels in Hypersonic Flow
Author:
Affiliation:
1. Ohio State University, Columbus, Ohio 43210
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054582
Reference47 articles.
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3. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
4. ZuchowskiB. “Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase I—Identification of Knowledge Gaps,” AFRL TR RB-WP-TR-2010-3069, Lockheed Martin Co. Aug. 2010.
5. ZuchowskiB. “Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase II—Detailed Design of Hypersonic Cruise Vehicle Hot-Structure,” AFRL TR RQ-WP-TR-2012-0280, Lockheed Martin Co. May 2012.
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