Data-driven modeling of hypersonic reentry flow with heat and mass transfer
Leonidas Gkimisis, Bruno Ricardo Barros Dias, James B. Scoggins,, Thierry Magin, Miguel Alfonso Mendez, Alessandro Turchi

TL;DR
This paper develops data-driven surrogate models for hypersonic reentry flows, enabling fast predictions of flow properties and surface quantities, which are crucial for aerospace design and analysis during reentry phases.
Contribution
It introduces physics-constrained neural network surrogate models trained on high-fidelity simulations for hypersonic flow prediction during reentry, including reactive and ablative surface modeling.
Findings
Surrogate models accurately predict flow variables along reentry trajectories.
Models effectively estimate surface quantities for nonreacting and ablative surfaces.
Validation shows high fidelity of surrogate predictions compared to detailed simulations.
Abstract
The entry phase constitutes a design driver for aerospace systems that include such a critical step. This phase is characterized by hypersonic flows encompassing multiscale phenomena that require advanced modeling capabilities. However, since high fidelity simulations are often computationally prohibitive, simplified models are needed in multidisciplinary analyses requiring fast predictions. This work proposes data-driven surrogate models to predict the flow, and mixture properties along the stagnation streamline of hypersonic flows past spherical objects. Surrogate models are designed to predict velocity, pressure, temperature, density and air composition as a function of the object's radius, velocity, reentry altitude and surface temperature. These models are trained with data produced by numerical simulation of the quasi-one-dimensional Navier-Stokes formulation and a selected Earth…
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Taxonomy
TopicsGas Dynamics and Kinetic Theory · Wind and Air Flow Studies · Radiative Heat Transfer Studies
