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A New Recycling Method to Generate Turbulent Inflow ProfilesThe accuracy of the scale-resolving simulations for practical geometries strongly depends on the inflow boundary conditions. Imposing experimentally observed turbulent inflow profiles for the numerical simulations is a major challenge. Existing methods available in the literature assume self-similar behavior, which is not true for most of the experiments. In the present work, we formulate the turbulent inflow profile generation technique as an optimization problem. An adjoint technique is exploited to evaluate the sensitivities of multiple input parameters for the present problem. The present formulation is then tested to generate a laminar boundary layer profile, turbulent boundary layer profile, and turbulent jet profile.
Document ID
20190026554
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Garai, Anirban
(Science and Technology Corp. Moffett Field, CA, United States)
Murman, Scott M.
(NASA Ames Research Center Moffett Field, CA, United States)
Ekelschot, Dirk
(Universities Space Research Association (USRA) Moffett Field, CA, United States)
Date Acquired
June 23, 2019
Publication Date
June 17, 2019
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARC-E-DAA-TN69970
Meeting Information
Meeting: AIAA Aviation 2019
Location: Dallas, TX
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: Airbus UK, American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNH15CO48B
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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