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Computational Modelling of Dynamic Stability Derivatives For Complete Aircraft Configuration Using Quasi Steady Frame Rotation

Asad Raza (195111)

Computational Modelling of Dynamic Stability Derivatives For Complete Aircraft Configuration Using Quasi Steady Frame Rotation - Kamra: Department of Aerospace Engineering, 2021. - 68 p.

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

Dewey Class. No.: 629.1 / ASA - MSAE

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