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5. WING AND TAILPLANE DESIGN 5.1 Maximum Lift Coefficient The maximum lift coefficient of the airplane C L,max depends upon many factors.Only the most important of these…

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NASA Technical Paper 2969 1990 NASA Supercritical Airfoils A Matrix of Family-Related Airfoils Charles Langley Hampton, D. Harris Research Virginia Center National Aeronautics-and…

Documents supercritical aerofoils

NASA Technical Paper 2969 1990 NASA Supercritical Airfoils A Matrix of Family-Related Airfoils Charles Langley Hampton, D. Harris Research Virginia Center National Aeronautics-and…

Documents Laminar Flow Rodney Bajnath, Beverly Beasley, Mike Cavanaugh AOE 4124 March 29, 2004.

Slide 1Laminar Flow Rodney Bajnath, Beverly Beasley, Mike Cavanaugh AOE 4124 March 29, 2004 Slide 2 Introduction Why laminar flow? –Less skin friction Lower drag Slide…