Wave Drag Reduction of SC(2)0410 Airfoil using New Developed Inviscid Compressible Adjoint Method

Wave Drag Reduction of SC(2)0410 Airfoil using New Developed Inviscid Compressible Adjoint Method

A supercritical airfoil is geometrically optimized using the new developed adjoint compressible lattice Boltzmann method. Minimizing the drag coefficient and eliminating the shock wave on the supercritical airfoil surface are considered as the cost function with constraint of fixed lift coefficient....

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Bibliographic Details
Main Authors: R. Kamali-Moghadam, H. Jalali, A. Haghiri
Format: Article
Language:English
Published: Isfahan University of Technology 2020-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
adjoint approach; aerodynamic shape optimization; transonic wind tunnel; supercritical airfoil; wave drag reduction; lattice boltzmann method.
Online Access:http://jafmonline.net/JournalArchive/download?file_ID=52930&issue_ID=1007

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