Flow Dynamics Past a 30P30N Three-Element Airfoil Using Improved Delayed Detached-Eddy Simulation
Author:
Affiliation:
1. University of Manchester, Manchester, England M13 9PL, United Kingdom
2. CD-adapco, London, England W6 7NL, United Kingdom
3. Carshalton, Surrey SM5 3SD, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054521
Reference17 articles.
1. Assessment of Slat Noise Predictions for 30P30N High-Lift Configuration from BANC-III Workshop
2. A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities
3. An Experimental Investigation of the 30P30N Multi-Element High-Lift Airfoil
4. Characterization of Unsteady Flow Structures Near Leading-Edge Slat: Part I: PIV Measurements
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