@inproceedings{1771c8672409450ca2e0128b530e5a70,
title = "Benchmarking the Langtry-Menter Transition Model Using OVERFLOW for the AIAA Transition Modeling Workshop",
abstract = "Several common test cases for validation of boundary-layer transition models are presented and benchmarked for the common Langtry-Menter transition model. Such standard test cases provide a suite of data for code verification and can be used similarly to investigate the inner workings of the transition model and provide guidance on model calibration. In this work, the NASA OVERFLOW 2.3d solver is employed to simulate and predict transition for two-dimensional and three-dimensional test cases, ranging from zero-pressure-gradient flat plates to full, three-dimensional wings with varying sweep. Results are compared quantitatively and qualitatively with experimental data along with existing computational data sets. Grid resolution studies are performed for some test cases to determine sensitivity to grid spacing with respect to transition prediction.",
author = "Carnes, {Jared A.} and Coder, {James G.}",
note = "Funding Information: This research was partially funded by the Government under Agreement No. W911W6-17-2-0003. The U.S. Government is authorized to reproduce and distribute reprints for Government purposes notwithstanding any copyright notation thereon. The views and conclusions contained in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the Aviation Development Directorate or the U.S Government. The authors would like to thank the Pennsylvania State University Vertical Lift Research Center of Excellence. The authors would also like to thank the AIAA Applied Aerodynamics Technical Committee{\textquoteright}s CFD Transition Modeling Discussion Group and also the AIAA Transition Modeling Workshop for providing the grids for this work. The authors thank Dr. B. Venkatachari (NIA) and Marie Denison (NASA) for their advice in debugging and post-processing the CRM-NLF simulations. Some images in this work were generated using FieldView, licenses for which were provided through their University Partners Program. Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA AVIATION 2022 Forum ; Conference date: 27-06-2022 Through 01-07-2022",
year = "2022",
doi = "10.2514/6.2022-3680",
language = "English (US)",
isbn = "9781624106354",
series = "AIAA AVIATION 2022 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA AVIATION 2022 Forum",
}