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Gradient Based Airfoil Shape Optimization to Improve Aerodynamic Performance of a Fighter Aircraft

Muhammad Usman Shahid (195114)

Gradient Based Airfoil Shape Optimization to Improve Aerodynamic Performance of a Fighter Aircraft - Kamra: Department of Aerospace Engineering, 2022. - 68 p.

Subjects--Topical Terms:
Department of Aerospace Engineering. (Thesis)

Dewey Class. No.: 629.1 / MUH - MSAE

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