A discrete adjoint framework for turbulent hypersonic flows in thermochemical nonequilibrium

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Abstract/Contents

Abstract
Hypersonic vehicle design and analysis continues to challenge the aerospace community. These systems operate in a unique flow environment characterized by thermochemical nonequilibrium effects, adding constraints and complexity not observed in other flow regimes. Numerical simulations must resolve these high-temperature, atomic-scale physical phenomena to accurately predict vehicle performance parameters such as lift, drag, control authority, and surface heat transfer. As a result, expensive CFD simulation models are substituted with low-fidelity correlation-based models in the design process. This yields, at best conservative vehicle configurations and, at worst, failed designs. Consequently, despite the rapid growth of computational power, hypersonic vehicle design has stagnated without the proper methods to efficiently incorporate CFD into the design process. This dissertation presents, to the author's knowledge, the first discrete adjoint framework for the efficient computation of aerothermodynamic sensitivities of turbulent hypersonic flows in thermochemical nonequilibrium to reintegrate high-fidelity simulations into the preliminary design phases for hypersonic vehicle systems.

Description

Type of resource text
Form electronic resource; remote; computer; online resource
Extent 1 online resource.
Place California
Place [Stanford, California]
Publisher [Stanford University]
Copyright date 2023; ©2023
Publication date 2023; 2023
Issuance monographic
Language English

Creators/Contributors

Author Maier, Walter Thomas
Degree supervisor Alonso, Juan José, 1968-
Thesis advisor Alonso, Juan José, 1968-
Thesis advisor Hara, Ken
Thesis advisor Lele, Sanjiva K. (Sanjiva Keshava), 1958-
Degree committee member Hara, Ken
Degree committee member Lele, Sanjiva K. (Sanjiva Keshava), 1958-
Associated with Stanford University, School of Engineering
Associated with Stanford University, Department of Aeronautics and Astronautics

Subjects

Genre Theses
Genre Text

Bibliographic information

Statement of responsibility Walter T. Maier.
Note Submitted to the Department of Aeronautics and Astronautics.
Thesis Thesis Ph.D. Stanford University 2023.
Location https://purl.stanford.edu/pj691zd1560

Access conditions

Copyright
© 2023 by Walter Thomas Maier

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