NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of anisotropic mesh adaptation on surface pressure predictions for atmospheric entry simulations.Recently, a metric-based mesh adaptation capability has been developed for the advanced compressible flow solver US3D. Metric-based mesh adaptation is a solution informed mesh adaptation strategy that typically improves the resolution of the mesh along anisotropic flow features, like strong shock waves or shear layers. An anisotropic error indicator is reconstructed based on a provided Computational Fluid Dynamics (CFD) solution which prescribes the locally desired element size and orientation. The benefits of this mesh adaptation strategy is twofold: first, it simplifies the manual meshing labor that typically needs to be carried out by the CFD engineer because the mesh adaptation is informed by the provided solution. Second, the computational cost is kept to a minimum while improving the resolution of the simulation.


The aim here is to demonstrate how anisotropic mesh adaptation can be employed to improve the predictions of surface pressure for atmospheric entry vehicles. In this work, we compare CFD simulations that use this newly developed anisotropic mesh adaptation capability for US3D with pressure data that was collected by Mars Entry, Descent, and Landing Instrumentation 2 (MEDLI2) during the atmospheric entry phase of Mars2020.
Document ID
20220009504
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
D. Ekelschot
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
J. M. Brock
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
June 17, 2022
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: Eleventh International Conference on Computational Fluid Dynamics (ICCFD) 2022
Location: Maui, Hawaii
Country: US
Start Date: July 11, 2022
End Date: July 15, 2022
Sponsors: University of California, Davis
Funding Number(s)
PROJECT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
No Preview Available