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 …

Multifidelity cokriging for high-dimensional output functions with application to hypersonic airloads computation

T Rokita, PP Friedmann - AIAA Journal, 2018 - arc.aiaa.org
An accurate surrogate model is capable of reproducing high-fidelity results at a fraction of
the computational cost. coKriging is an efficient method for constructing surrogate models …

Physics-Infused Reduced-Order Modeling of Aerothermal Loads for Hypersonic Aerothermoelastic Analysis

C Vargas Venegas, D Huang - AIAA journal, 2023 - arc.aiaa.org
This paper presents a novel physics-infused reduced-order modeling (PIROM) methodology
for efficient and accurate modeling of nonlinear dynamical systems. The PIROM consists of a …

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 …

Expedient hypersonic aerothermal prediction for aerothermoelastic analysis via field inversion and machine learning

CA Vargas Venegas, D Huang - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1707. vid The accurate and
efficient prediction of aerothermal loads over the hypersonic vehicles during atmospheric …

Considerations for a hypersonic flight test investigating fluid-thermal-structural interactions

LP McQuellin, A Neely, G Currao - 23rd AIAA International Space …, 2020 - arc.aiaa.org
Sustained hypersonic flight remains a state-of-the-art problem, with limited examples of
vehicles capable of performing in this extreme environment for extended periods of time …

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 …

Physics-Infused Reduced Order Modeling of Hypersonic Aerothermal Loads for Aerothermoelastic Analysis

CA Vargas Venegas, D Huang - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0989. vid This paper presents the
Physics-Infused Reduced Order Modeling (PIROM) methodology. It integrates 1) a physics …

[PDF][PDF] Efficient reduced-order modeling for skin panels in hypersonic flow and its application to generating aerothermoelastic scaling laws

D Huang, T Rokita, PP Friedmann - International Forum on …, 2017 - researchgate.net
This study describes the development of an efficient aerothermoelastic computational
framework and its application to aerothermoelastic scaling law development. In the …

Reliability analysis of a hypersonic vehicle panel with spatio-temporal variability

Z Hu, S Mahadevan - AIAA Journal, 2019 - arc.aiaa.org
Coupled aerothermoelastic analysis is required to predict the response of a hypersonic
vehicle panel. The required computational effort of the coupled multidisciplinary analysis …