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Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow

The flight performance of aircraft relies on aerodynamic non-dimensional parameters like the drag coefficient, lift coefficient, and the moment coefficient of the aerospace vehicles. The knowledge of these properties is supremely necessary for optimal design, and thus the aerodynamics and the perfo...

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書誌詳細
主要な著者:	SHAMITHA, A, Crasta, Asha, Khan, Sher Afghan, VASAVI, P
フォーマット:	論文
言語:	English
出版事項:	TJPRC Pvt. Ltd 2020
主題:	TL787 Astronautics
オンライン･アクセス:	http://irep.iium.edu.my/80867/1/22splissuejun2020ijmperd22j.pdf http://irep.iium.edu.my/80867/ http://www.tjprc.org/journals/journal-of-mechanical-engineering
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