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Pressure distribution at Mach numbers up to 0.90 on a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10, including the effects of fences

Frederick W. Boltz, Harry H Shibata

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Key concepts: Wing, Mach number, Distribution (mathematics), Aspect ratio (aeronautics), Wing loading, Mathematics, Mechanics, Physics

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Pressure distribution at Mach numbers up to 0.90 on a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10, including the effects of fences — Research Paper | ScholarLens