Pressure distribution guided supercritical wing optimization
نویسندگان
چکیده
منابع مشابه
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Extensive wind tunnel tests are conducted to evaluate surface pressure distribution of a semi span swept wing. The wing section has a laminar flow airfoil similar to NACA 6-series airfoils. The investigations are conducted at various speeds and angles of attack. Surface pressure distribution over the wing upper surface is measured for both chordwise and spanwise sections. Statistical analyses a...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2018
ISSN: 1000-9361
DOI: 10.1016/j.cja.2018.06.021