Shock Waves 2009
DOI: 10.1007/978-3-540-85181-3_85
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Wave processes on a supercritical airfoil

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“…The aerofoil geometry selected for these tests was the supercritical aerofoil BAC 3-11 with 11% of maximum thickness. This aerofoil experiences shock buffet conditions at Mach numbers between [0.75-0.88], at low angles of attack [0-5°] and at Reynolds numbers ranging between two and three millions (5,6,7).…”
Section: Introductionmentioning
confidence: 99%
“…The aerofoil geometry selected for these tests was the supercritical aerofoil BAC 3-11 with 11% of maximum thickness. This aerofoil experiences shock buffet conditions at Mach numbers between [0.75-0.88], at low angles of attack [0-5°] and at Reynolds numbers ranging between two and three millions (5,6,7).…”
Section: Introductionmentioning
confidence: 99%