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 …
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 …
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
Flutter onset characteristic is an important consideration for transport aircraft design.
Previous work with high fidelity aerostructural optimization has shown a tendency for …
Previous work with high fidelity aerostructural optimization has shown a tendency for …
Aerothermoelastic scaling laws for hypersonic skin panel configurations with arbitrary flow orientation
This study describes the development of an efficient aerothermoelastic computational
framework and its application to the aerothermoelastic scaling law development. In the …
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 …
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
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 …
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 …
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 …
hypersonic aerothermoelastic scaling laws using a novel two-pronged approach. The …