Panel Response Prediction Through Reduced Order Models with Application to Hypersonic Aircraft-Reference-Cited by-同舟云学术

Panel Response Prediction Through Reduced Order Models with Application to Hypersonic Aircraft

Published:2015-01-02 Issue: Volume: Page:
ISSN:
Container-title:56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Mignolet Marc P.¹,Culler Adam J.²,McNamara Jack J.³,Matney Andrew¹,Spottswood Stephen M.⁴

Affiliation:

1. Arizona State University

2. Sierra Lobo, Inc.

3. Ohio State University

4. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1630

Reference16 articles.

1. B. Zuchowski, "Predictive Capability for Hypersonic Structural Response and Life Prediction, Phase 1 - Identification of Knowledge Gaps," Technical Report, AFRL-RB-WPTR-2010-3069, August 2010.

2. Coupled Flow-Thermal-Structural Analysis for Response Prediction of Hypersonic Vehicle Skin Panels

3. Fluid-Thermal Response of Spherical Dome Under a Mach 6.59 Laminar Boundary Layer

4. Impact of Fluid-Thermal-Structural Coupling on Response Prediction of Hypersonic Skin Panels

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