@article{712d67fb30c348e297c991d7811e53e5,
title = "Aerothermoelastic scaling laws for hypersonic skin panel configurations with arbitrary flow orientation",
abstract = "This study describes the development of an efficient aerothermoelastic computational framework and its application to the aerothermoelastic scaling law development. In the framework, a novel approach is developed for the reduced-order model of the fluid solver, which accounts for nonuniform temperature distribution and geometrical scales using simple analytical pointwise models. Subsequently, a new, two-pronged approach to aerothermoelastic scaling is presented. It combines the classical scaling approach with augmentation from numerical simulations of the specific problem. This enables one to obtain useful scaling information for important quantities that cannot be treated by the classical approach. Finally, the framework is applied to study the effect of flow orientation angle on panel flutter and the development of a scaling law for a hypersonic skin panel configuration.",
author = "Daning Huang and Friedmann, {Peretz P.} and Tomer Rokita",
note = "Funding Information: This research was funded by the Fran{\c c}ois-Xavier Bagnoud Center for Rotary and Fixed Wing Air Vehicle Design. In addition, D. Huang gratefully acknowledges the support of the Rackham Predoctoral Fellowship awarded by the University of Michigan, and T. Rokita gratefully acknowledges the support of the Postdoctoral Research Fellowship awarded by the University of Michigan. Funding Information: This research was funded by the Fran?ois-Xavier Bagnoud Center for Rotary and Fixed Wing Air Vehicle Design. In addition, D. Huang gratefully acknowledges the support of the Rackham Predoctoral Fellowship awarded by the University of Michigan, and T. Rokita gratefully acknowledges the support of the Postdoctoral Research Fellowship awarded by the University of Michigan. Publisher Copyright: {\textcopyright} 2018 by D. Huang, P. P. Friedmann, and T. Rokita. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.",
year = "2019",
doi = "10.2514/1.J057499",
language = "English (US)",
volume = "57",
pages = "4377--4392",
journal = "AIAA Journal",
issn = "0001-1452",
publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",
number = "10",
}