Computational Fluid Dynamics Analyses for the High-Lift Common Research Model Using the USM3D and FUN3D Flow Solvers
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0320
Reference12 articles.
1. Lacy, D.S., and Sclafani, A.J. "Development of the High-Lift Common Research Model (HL-CRM): A Representative High Lift Configuration for Transonic Transports, AIAA Paper 2016-0308, January 2016.
2. Development of a Common Research Model for Applied CFD Validation Studies
3. 4Pandya, M., Abdol-Hamid, K., Campbell, R., and Frink, N. "Implementation of Flow Tripping Capability in the USM3D Unstructured Flow Solver". AIAA-2006-919, January 2006.
4. 5Pandya, M., Frink, N., and Noack, R. "Progress Toward Overset-Grid Moving Body Capability for USM3D Unstructured Flow Solver". AIAA-2005-5118, June 2005.
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