Movi-ng-Surface Boundary-Layer Control for Aircraft Operation at High Incidence

Modi, V. J.; Sun, Jiacun; Akutsu, Toshinosuke; Lake, P. S.; McMillan, Kate; Swinton, P.; Mullins, David R.

doi:10.2514/3.57587

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Cited by 46 publications

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“…There are many ways to control of boundary likes using devices to control boundary layer or using very small extended surfaces starting from body that want to control the boundary layer on. Modi [2,3] presented a comprehensive wind-tunnel test program involving a family of airfoils such as NACA 63-218 and Joukowsky with one or more cylinders forming the moving surface. Their results suggested that the leading-edge rotating cylinder increases the maximum lift coefficient and delays the stall angle of attack by (2.73 and 48°), respectively.…”

Section: Introductionmentioning

confidence: 99%