Projects and Grants per year
Grants and Contracts Details
Description
Modeling entry of spacecrafts is a challenging because of the vast number of dierent
physical phenomena that occur during the process. However, in order to size thermal
protection systems, engineers rely on high delity solvers to provide accurate predictions
of both the thermochemical environment surrounding the heat shield, and its material
response. Before using the aerothermodynamics and thermal response solvers for design,
it is necessary to guarantee that the models are implemented correctly through veri-
cation, and that the implemented models correspond to the real physical phenomena
through validation.
The work proposes an extensive verication and validation of two solvers: KATS, a
computational
uid dynamics and material response solver developed at the University
of Kentucky, and Icarus, a new material response solver developed at NASA Ames.
The verication will encompass the development of an automated regression testing
tool to both aid code developers in the debugging process, as well as verify the correct
implementation of the numerical models as these are developed. This will be performed
through comparison to analytical solutions, when these are known, and to solutions
using method of manufactured solutions (MMS) when they are not. The validation
process will be performed through comparison to relevant ablation experiments, namely
arc-jet tests. The rst test-set will be from the experiments run at NASA Ames by Milos
and Chen, on PICA. This comparison consists of material recession measurements and
temperature proles from thermocouple measurements at dierent locations on Iso-Q
samples. The second test-set is obtained from the recent experiments performed at the
NASA HYMETS facility on FiberForm, where material recession measurements were
taken.
The successful completion of the project will not only provide the extensive verica-
tion and validation of two separate codes but will also establish a work-
ow streamline
between two separate codes, where KATS can serve as a model testing tool for Icarus,
whose main function will be for design.
Status | Finished |
---|---|
Effective start/end date | 1/1/17 → 7/31/18 |
Funding
- National Aeronautics and Space Administration
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Projects
- 1 Finished
-
National Space Grant College and Fellowship Program (SPACE Grant) Training Grant 2015-2018
Smith, S. (PI) & Hayes, J. (CoI)
National Aeronautics and Space Administration
8/4/15 → 2/3/21
Project: Research project