Application of the adjoint optimisation of shock control bump for ONERA-M6 wing
Author:
Affiliation:
1. Aerospace Engineering, Science and Research Branch of Islamic Azad University, Tehran, Iran
2. Aerospace Engineering, Sharif University of Technology, Tehran, Iran
Publisher
River Publishers
Subject
Mechanical Engineering,Mechanics of Materials,Modelling and Simulation
Link
https://www.tandfonline.com/doi/pdf/10.1080/17797179.2017.1386022
Reference24 articles.
1. Large-Eddy Simulation of Shock/Boundary-Layer Interaction
2. Compressible flow characteristics around a biconvex arc airfoil in a channel
3. Experimental Study into the Flow Physics of Three-Dimensional Shock Control Bumps
4. Joint Experimental and Numerical Approach to Three-Dimensional Shock Control Bump Research
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