Design of Thermally Stressed Panels Subject to Transonic Flutter Constraints-Reference-Cited by-同舟云学术

Design of Thermally Stressed Panels Subject to Transonic Flutter Constraints

Published:2017-11 Issue:6 Volume:54 Page:2340-2349
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Bhatia Manav¹,Beran Philip¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Dayton, Ohio 45433

Funder

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.C034301

Reference22 articles.

1. BhatiaM. “Design-Oriented Thermoelastic Analysis, Sensitivities, and Approximations for Shape Optimization of Aerospace Vehicles,” Ph.D. Thesis, Univ. of Washington, Seattle, WA, 2007.

2. Design-Oriented Thermostructural Analysis with Internal and External Radiation, Part 1: Steady State

3. Design-Oriented Thermostructural Analysis with External and Internal Radiation, Part 2: Transient Response

4. DeatonJ. D. “Design of Thermal Structures Using Topology Optimization,” Ph.D. Thesis, Wright State Univ., Dayton, OH, 2009.

5. Aerothermoelastic topology optimization with flutter and buckling metrics

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