Parametric Exploration of Wing–Body Junction Flow Using Computational Fluid Dynamics
Author:
Affiliation:
1. Beechcraft Corporation, Wichita, Kansas 67206
2. Department of Aerospace Engineering, Wichita State University, Wichita, Kansas 67260
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032985
Reference20 articles.
1. Time-depeiident and time-averaged turbulence structure near the nose of a wing-body junction
2. JUNCTION FLOWS
3. Experimental transport-rate budgets in complex 3-D turbulent flow near a wing-body junction
4. Modification of junction flows by altering the section shapes of the cylinders
5. Influence of Wing Shapes on Surface Pressure Fluctuations at Wing-Body Junctions
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1. A hybrid RANS model of wing-body junction flow;European Journal of Mechanics - B/Fluids;2020-01
2. Using an Anti-Fairing to Reduce Drag at Wing/Body Junctions;AIAA Journal;2019-04
3. Experimental and Computational Analysis of Model–Support Interference in Low-Speed Wind-Tunnel Testing of Fuselage-Boundary-Layer Ingestion;MATEC Web of Conferences;2019
4. Efficient suction control of unsteadiness of turbulent wing-plate junction flows;Journal of Hydrodynamics;2017-04
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