Abstract
The paper deals with the problem of thin aerofoil with multiple slotted movable hinge flaps. Two particular cases are considered: a) assuming no gaps exist at the hinges, and b) considering the existence of slots. The conventional assumptions of small angle of attack, small flap deflection and small camber are omitted.
References
T. S. PATEL, Thin aerofoil theory applied to the wing with a rotating flap, Soviet Aeronautics, 4, 1970.
T. S. PATEL, Wing profile with a rotating flap in the flow with velocity gradient near ground surface, Sbornik Nauchnikh Rabot, Mekhanika, M.S.U, 1, 1973 [in Russian].
E. L. HOUGHTON and N. B. CARRUTHERS, Aerodynamics for engineering students, E. Arnold Publ., London 1982.
T. A. DERBASI and A. N. HASSANEN, Thin aerofoil theory applied to the wing double slotted flaps, Project Report, Dept. of Aero. Eng., Al-Fateh University, 1985.
H. MULTROPP, Methods for calculating lift distribution of wing, ARC R and M, 2884, England. 1950.
T. S. PATEL, Wing profile with a rotating flap in the flow with velocity gradient near ground surface, Sbornik Nauchnikh Rabot, Mekhanika, M.S.U, 1, 1973 [in Russian].
E. L. HOUGHTON and N. B. CARRUTHERS, Aerodynamics for engineering students, E. Arnold Publ., London 1982.
T. A. DERBASI and A. N. HASSANEN, Thin aerofoil theory applied to the wing double slotted flaps, Project Report, Dept. of Aero. Eng., Al-Fateh University, 1985.
H. MULTROPP, Methods for calculating lift distribution of wing, ARC R and M, 2884, England. 1950.
