An aerothermoelastic analysis framework with reduced-order modeling applied to composite panels in hypersonic flows

D Huang, PP Friedmann - Journal of Fluids and Structures, 2020 - Elsevier
This study describes the enhancement of a computational framework for
aerothermoelasticity using novel model order reduction techniques and efficient coupling …

Development of a hypersonic aerothermoelastic framework and its application to flutter and aerothermoelastic scaling of skin panels

D Huang - 2019 - deepblue.lib.umich.edu
In the past decade, there has been a strong interest in reusable air-breathing hypersonic
vehicles for in both civil and military applications. However, there are still the unresolved …

A coupled newton-krylov time spectral solver for wing flutter and lco prediction

S He, E Jonsson, CA Mader, JRRA Martins - AIAA Aviation 2019 Forum, 2019 - arc.aiaa.org
Flutter onset characteristic is an important consideration for transport aircraft design.
Previous work with high fidelity aerostructural optimization has shown a tendency for …

Aerothermoelastic scaling laws for hypersonic skin panel configurations with arbitrary flow orientation

D Huang, PP Friedmann, T Rokita - AIAA journal, 2019 - arc.aiaa.org
This study describes the development of an efficient aerothermoelastic computational
framework and its application to the aerothermoelastic scaling law development. In the …

A surrogate-based optimization framework for hypersonic aerothermoelastic scaling laws with application to skin panels

D Huang, PP Friedmann - AIAA SciTech 2019 Forum, 2019 - arc.aiaa.org
This study describes the development of an optimization framework for generating
hypersonic aerothermoelastic scaling laws using a novel two-pronged approach. The …

Impact of high-temperature effects on the aerothermoelastic behavior of composite skin panels in hypersonic flow

A Sadagopan, D Huang, KM Hanquist - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
This study investigates the impact of the high-temperature effect, esp. the real gas effect and
the chemical reactions, on hypersonic aerothermodynamic solutions and the …

[图书][B] Assessment of Reduced Fidelity Modeling of a Maneuvering Hypersonic Vehicle

ER Dreyer - 2021 - search.proquest.com
Balancing accurate and efficient estimation of aerothermodynamic loads is a significant
challenge for multi-disciplinary modeling and analysis of high speed vehicles. High fidelity …

A multi-objective optimization framework for hypersonic aerothermoelastic scaling laws and its application to skin panels

D Huang, PP Friedmann - International Forum on Aeroelasticity and …, 2019 - pure.psu.edu
This study describes the development of an optimization framework for generating
hypersonic aerothermoelastic scaling laws using a novel two-pronged approach. The …