NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
The State of Scale-Resolving Simulations for Aircraft High-Lift Applications: Summary of the Closing Discussion of the 2025 NASA High-Fidelity CFD WorkshopA thorough and robust discussion was held during the last session of the 2025 NASA CFD High-fidelity Workshop, regarding the success of the current RCA Technical Challenge (TC): to ‘Develop and demonstrate computationally efficient, eddy-resolving modeling tools that predict maximum lift coefficient for transport aircraft with the same accuracy as certification flight tests.’ The consensus of the delegates was that significant progress towards achieving the TC has been demonstrated, particularly through the collaborative development and use of Wall-Modeled Large-Eddy Simulation (WMLES). The remaining tasks required to fully meet the TC were highlighted. No consensus was reached regarding possible topics for a new RCA TC. However, many opinions were expressed and captured, and key emerging technologies that will likely affect it were discussed.
Document ID
20250006712
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Gary Coleman
(Langley Research Center Hampton, United States)
Mujeeb Malik
(Langley Research Center Hampton, United States)
Chris Rumsey
(Langley Research Center Hampton, United States)
Jeff Slotnick
(Boeing (United States) Chicago, United States)
Date Acquired
July 1, 2025
Publication Date
July 1, 2025
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-20250006712
Funding Number(s)
PROJECT: 109492.02.07.05.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Computational Fluid Dynamics
No Preview Available