Engineering Transactions, 36, 1, pp. 3-14, 1988

Thin Aerofoil with Multiple Slotted Flap

T.S. Patel
Al-Fateh University, Tripoli
Libya

T.A. Derbasi
Al-Fateh University, Tripoli
Libya

A.N. Hassanen
Al-Fateh University, Tripoli
Libya

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.

Full Text: PDF

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.




Copyright © 2014 by Institute of Fundamental Technological Research
Polish Academy of Sciences, Warsaw, Poland