Stall Flutter of a Thin Aerofoil with Leading Edge Separation
نویسندگان
چکیده
منابع مشابه
The Formation of Regions of Separated Flow on Wing Surfaces Part I Low - Speed Tests on a Two - Dimensional Unswept Wing
Tests of a two-dimensional straight wing with a 10 per cent thick RAE 101 section have been made in a low-speed wind tunnel to check the validity of a criterion suggested by Owen and Klanfer for the type of bubble which will be formed when a laminar boundary layer separates from the surface of an aerofoil. The results confirm this hypothesis and show that if the boundary-layer Reynolds number b...
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ژورنال
عنوان ژورنال: Bulletin of JSME
سال: 1974
ISSN: 0021-3764,1881-1426
DOI: 10.1299/jsme1958.17.578