Drag Prediction in Transitional Flow Over Airfoils

Author:

Basha Wassim A.1,Ghaly Wahid S.1

Affiliation:

1. Concordia University, Montreal, Quebec H3G 1M8, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical investigation of transitional flows over NACA 0012 Airfoil;Lecture Notes in Mechanical Engineering;2023

2. A FEniCS-based model for prediction of boundary layer transition in low-speed aerodynamic flows;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-06-12

3. Verification, Validation, and Application of Shear Stress Transport Transitional Model to a R/C Aircraft;2018 AIAA Aerospace Sciences Meeting;2018-01-07

4. A comprehensive review of the theoretical approaches for the airfoil design of lift-type vertical axis wind turbine;Renewable and Sustainable Energy Reviews;2015-11

5. Aerodynamic Shape Optimization of Natural Laminar Flow (NLF) Airfoils;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

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