The NASA Juncture Flow test, whose purpose is CFD validation for wing juncture trailing edge separation and progression, was designed from the outset to be a highly collaborative effort between CFD computationalists and experimentalists. This paper highlights key aspects of the planning and execution of the project, which has recently completed its first phase of wind tunnel testing. The joint CFD/experimental team is described, and its accomplishments to date are summarized.
The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration
AIAA Aviation and Aeronautics Forum and Exposition ; 2018 ; Atlanta, GA, United States
2018-06-25
Conference paper
No indication
English
The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration (AIAA 2018-3319)
British Library Conference Proceedings | 2018
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