Arrangement for controlling the air flow over aerodynamic profil

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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416 91, B64C 2102

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active

046417990

ABSTRACT:
An arrangement for controlling the air flow past an aerodynamic profile, (such as an aerofoil surface of a wing, tail plane, or fuselage of an aircraft or missile, a propeller, helicopter rotor, or blading of a turbo-engine fan or wind impeller) by providing a number of orifices of small diameter spaced apart in the profile surface in the longitudinal direction of the profile transversely to the direction of air flow over the profile and to the chordwise direction of the profile. Fluid is either discharged or drawn in through the orifices perpendicularly to the air flow in the region of separation of laminar flow. The orifices have a coefficient of flow (i.e., either a discharge or an intake coefficient) C.sub.Q =(V/FV) of up to 10.sup.-4 for a Reynolds Number less than 3.times.10.sup.6, where v=volume flow of the fluid through the discharge orifices, F=profile area and V=velocity of the air stream flowing over the wing or blade. The invention is particularly concerned with controlling the air flow over an aerofoil profile of a wing of a slowly flying aircraft, such as a glider or light aircraft.

REFERENCES:
patent: 2833492 (1958-05-01), Fowler
patent: 3194518 (1965-07-01), Walsh
patent: 3262658 (1966-07-01), Reilly
patent: 3421577 (1969-01-01), Valyi
patent: 4033526 (1977-07-01), Benson
"Flight Experiments on Suction for High Lift", by M. R. Head et al., Jour of Aircraft, vol. 4, Mar./Apr. 1967, pp. 81-89.
"Low-Speed Flows Involving Bubble Separations", by Itiro Tani, Progress in Aeronautical Sciences, vol. 5, 1964, pp. 70-81.

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