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Influences of propeller advance ratio on delta-winged uav model vortex properties

The flow above the upper surface of delta wing is dominated by a very complicated and unresolved vortex structure. This study investigates the effects of the propeller advance ratio on the vortex properties and vortex breakdown above a generic 55° sharp-edged non-slender delta wing UAV model. The ex...

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書誌詳細
主要な著者:	Ramalingam, Santhoshinii, Mat, Shabudin, Kasim, Khushairi Amri, Said, Mazuriah, Mohd. Nasir, Mohd. Nazri, Nik Mohd., Nik Ahmad Ridhwan, Mansor, Shuhaimi, Mohamed Radzi, Nor Haizan, Perumal, Kannan
フォーマット:	論文
出版事項:	The Aeronautical and Astronautical Society of the Republic of China 2019
主題:	TJ Mechanical engineering and machinery
オンライン･アクセス:	http://eprints.utm.my/id/eprint/88554/ http://dx.doi.org/10.6125/JoAAA.201906_51(2).04
タグ:	タグ追加タグなし, このレコードへの初めてのタグを付けませんか!

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