关注
Kyle Thompson
Kyle Thompson
NASA Langley Research Center
在 nasa.gov 的电子邮件经过验证
标题
引用次数
引用次数
年份
FUN3D Manual: 13.7
RT Biedron, JR Carlson, JM Derlaga, PA Gnoffo, DP Hammond, ...
3112020
Sketch-to-solution: An exploration of viscous CFD with automatic grids
WL Kleb, MA Park, WA Wood, KL Bibb, KB Thompson, RJ Gomez
AIAA Aviation 2019 Forum, 2948, 2019
632019
FUN3D Manual: 14.1
WK Anderson, RT Biedron, JR Carlson, JM Derlaga, B Diskin, ...
452024
LAURA users manual: 5.6
KB Thompson, BR Hollis, CO Johnston, B Kleb, VR Lessard, A Mazaheri
452020
Recent Improvements to the LAURA and HARA Codes
KB Thompson, CO Johnston, BR Hollis, V Lessard
AIAA Aviation 2020 Forum, 3030, 2020
132020
Streamlined Convergence Acceleration for CFD Codes
KB Thompson, M O'Connell
AIAA Aviation 2019 Forum, 3709, 2019
122019
Application of the dependency inversion principle to multidisciplinary software development
M O'Connell, C Druyor, KB Thompson, K Jacobson, WK Anderson, ...
2018 fluid dynamics conference, 3856, 2018
112018
Aerothermodynamic Analyses for the LOFTID Technology Demonstration Mission
BR Hollis, AJ Wise, DS Liechty, AM Korzun, KB Thompson, NS Rodrigues, ...
AIAA SciTech 2024 Forum, 1498, 2024
102024
Economical Third-Order Methods for Accurate Surface Heating Predictions on Simplex Element Meshes
KB Thompson, H Nishikawa, E Padway
AIAA SCITECH 2023 Forum, 2629, 2023
102023
T-infinity: The Dependency Inversion Principle for Rapid and Sustainable Multidisciplinary Software Development
MD O'Connell, CT Druyor, KB Thompson, KE Jacobson, WK Anderson, ...
AIAA 2018 Aviation Meeting, 2018
72018
Towards an Automated Unstructured Grid Adaptation Workflow with VULCAN
M O'Connell, JA White, KB Thompson
AIAA AVIATION 2021 FORUM, 2701, 2021
62021
Simulation of a variety of wings using a Reynolds stress model
KB Thompson, HA Hassan
Journal of Aircraft 52 (5), 1668-1680, 2015
62015
A Decoupled Method for the Roe FDS Scheme in the Reacting Gas Path of FUN3D
KB Thompson, PA Gnoffo
54th AIAA Aerospace Sciences Meeting, 2062, 2016
52016
Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation
KB Thompson
North Carolina State University, 2017
42017
Improvements to the LAURA Mesh Adaptation Algorithm
KB Thompson, AJ Wise, BR Hollis
AIAA AVIATION 2023 Forum, 4332, 2023
32023
Tapping the brake for entry, descent, and landing
PA Gnoffo, K Thompson, A Korzun
46th AIAA Fluid Dynamics Conference, 4277, 2016
22016
The effects of dehydration status on cognitive functioning and perceptions of effort
N Callow, L Hardy, A Rowlands, S Worth, G Parfitt, K Thompson, M Cook, ...
Journal of Sports Sciences 21 (4), 264-265, 2003
22003
Assessment of Radiation Scattering by Dust in Mars Entry
A Hinkle, CO Johnston, KB Thompson, S Hosder
AIAA SCITECH 2025 Forum, 1535, 2025
2025
Experimental and Computational Study of Convective Heating on the Aeroshell Back Side and Payload of the LOFTID Vehicle
BR Hollis, EF Rieken, KB Thompson, AJ Wise, KE Hollingsworth, ...
National Aeronautics and Space Administration, 2024
2024
Validation of the HyperSolve CFD Solver for Entry Descent and Landing Applications
KB Thompson, MD O'Connell, AD Hinkle, C Pederson
AIAA SCITECH 2024 Forum, 1973, 2024
2024
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