Performance of Transition-Sensitive Models in Predicting Flow Structures over Delta Wings
Author:
Affiliation:
1. Department of Industrial and Mechanical Engineering, Lebanese American University, Byblos, Lebanon
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032601
Reference23 articles.
1. Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number
2. GordnierR. E.VisbalM. “Higher-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow,” AIAA Paper 2003-0620, Jan. 2003.
3. High-Order-Accurate Methods for Complex Unsteady Subsonic Flows
4. On the Use of Higher-Order Finite-Difference Schemes on Curvilinear and Deforming Meshes
5. Buffeting Flows over a Low-Sweep Delta Wing
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1. Experimental and Numerical Simulation Research on Boundary Layer Transition Front over a Swept Wing at M = 6;Fluid Dynamics;2021-05
2. Correlation-Based Transition Model for Swept-Wing Flow Using the Cross-Flow Reynolds Number;Journal of Aircraft;2017-01
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