Linear Reduced-Order Model of Airfoil Gust Response
نویسندگان
چکیده
منابع مشابه
Airfoil-Gust Interactions in Transonic Flow
Leading edge noise is a significant broadband noise source in aircraft engines, and is the primary broadband noise mechanism in outlet guide vane noise in turbofans, and broadband rotor wake interaction noise in contra-rotating open rotor engines. Previous authors have studied the effects of various aspects relating to this noise source, including airfoil geometry effects, cascade effects, and ...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 2019
ISSN: 0021-8669,1533-3868
DOI: 10.2514/1.c035011