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Laminar airfoil suitable for general-purpose aircraft and with focus on cruise characteristic

A cruising characteristic, laminar flow wing technology, applied in the directions 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 lift, and high cruise efficiency.

Active Publication Date: 2017-06-20
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, it is still only a low-speed constant-lift single-working-condition design, and there is no research on the performance of multiple working conditions.

Method used

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  • Laminar airfoil suitable for general-purpose aircraft and with focus on cruise characteristic
  • Laminar airfoil suitable for general-purpose aircraft and with focus on cruise characteristic
  • Laminar airfoil suitable for general-purpose aircraft and with focus on cruise characteristic

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Embodiment Construction

[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 object of the invention is to propose a laminar flow airfoil suitable for general-purpose aircraft, which pays more attention to the cruising 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 fact that the cruising and climbing states are dominated by laminar flow, the airfoil design is carried out according to the idea of ​​emphasizing the cruising characteristics, and the index requirements are:

[0041] 1. The length of the laminar flow zone...

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Abstract

The invention provides a laminar airfoil TFNLF3 with focus on a cruise characteristic and with a maximum relative thickness of 0.17 by adopting a computational fluid dynamics method and an airfoil parametrization method based on the NLF0416 airfoil which is published internationally and with consideration to cruise, climbing and stall for the design state and. The radius of the leading edge of the laminar airfoil TFNLF3 is 2.14%C; the maximum thickness of the same is 17.22%C; the location of the maximum thickness is 40.42% C; the maximum camber of the same is 1.35%C; the location of the maximum camber is 82.19% C; the thickness of the trailing edge of the laminar airfoil TFNLF3 is 0.42%C; and C is the chord length of the laminar airfoil TFNLF3. Under the circumstance that the stall and climbing performance is maintained or is slightly better than that of the NLF0416 airfoil, the laminar airfoil TFNLF3 has the advantages of better improving the cruise performance, increasing the cruising lift-to-drag ratio to a certain extent, reducing the absolute value of the cruising moment and reducing the cruising trim drag. When the cruise state is mainly controlled by laminar flow, the length of the flow region of an upper airfoil surface is 45% and the length of the flow region of a lower airfoil surface is 65%.

Description

technical field [0001] The invention relates to the field of airfoil design in the aerodynamic shape design of aviation aircraft, in particular to a laminar flow airfoil suitable for general-purpose aircraft with emphasis on cruising characteristics. Background technique [0002] General-purpose aircraft refers to all other civil aircraft except regular airline flights for passenger and cargo transportation. Its application fields include industry, agriculture, forestry, scientific research, tourism, sports, urban management and ambulance, training and official flight, etc. Referring to the experience of developed countries, general aviation, as an important part of the civil aviation industry, plays a great role in promoting the country's economic development and urban transportation. With the strengthening of our country's national strength and the improvement of people's income, following the popularization of automobiles, we will soon enter a period of rapid development ...

Claims

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Application Information

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IPC IPC(8): B64C3/14
CPCB64C3/14B64C2003/142
Inventor 张煜白俊强何小龙杨一雄李立
Owner NORTHWESTERN POLYTECHNICAL UNIV
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