Laminar flow aerofoil profile with emphasis on stall characteristic applicable to common aero vehicle
A stall characteristic, laminar flow wing technology, applied in the direction of wings, aircraft parts, wing shapes, etc., can solve the problem of lack of research on multi-working conditions performance, and achieve the effects of high lift-to-drag ratio, high cruise efficiency, and high lift.
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[0038] Embodiments of the present invention are described in detail below, and the embodiments are exemplary and intended to explain the present invention, but should not be construed as limiting the present invention.
[0039] The purpose of the invention is to propose a laminar flow airfoil suitable for general-purpose aircraft, which pays more attention to the stall characteristics of the airfoil while meeting the performance design requirements.
[0040] Through the use of advanced airfoil design and optimization technology, the airfoil can have a higher lift-to-drag ratio at a lower design lift coefficient, lower flight Mach number and lower flight Reynolds number, thereby improving cruise efficiency . In view of the situation that laminar flow is the main control in the cruising and climbing states, the airfoil design is carried out according to the idea of emphasizing the stall characteristics, and the index requirements are:
[0041] 1. The length of the laminar flo...
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