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

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TextPublication details: Kamra: Department of Aerospace Engineering, 2021.Description: 68 pSubject(s):

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Holdings
Item type	Current library	Call number	Status	Barcode
Thesis	Air University Kamra Campus Library	629.1 ASA - MSAE (Browse shelf(Opens below))	Available	THKC0014

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