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Method for processing airfoil surface load

A processing method and airfoil technology, applied in the field of aircraft, can solve the problem of neglecting the load distribution pattern and so on

Active Publication Date: 2015-09-23
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] In the existing technology, the total load and the total moment before and after the load treatment are usually compared, and the error after treatment is controlled at 5%, and if it exceeds 5%, it will be corrected, ignoring the load distribution form, and there are certain limitations

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  • Method for processing airfoil surface load
  • Method for processing airfoil surface load
  • Method for processing airfoil surface load

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Embodiment Construction

[0022] To make the objectives, technical solutions, and advantages of the implementation of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the accompanying drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals indicate the same or similar elements or elements with the same or similar functions. The described embodiments are part of the embodiments of the present invention, but not all of the embodiments. The embodiments described below with reference to the accompanying drawings are exemplary, and are intended to explain the present invention, but should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention. The ...

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Abstract

The invention discloses a method for processing airfoil surface load, which comprises the steps as follows: step 1: applying pressure on an airfoil surface to be measured; step 2: forming a pressure distribution three-dimensional model of the airfoil surface to be measured so as to obtain functional relationship in the pressure distribution three-dimensional model; step 3: forming a finite element planar model of the airfoil surface to be measured; step 4: mapping the finite element planar model of the airfoil surface to be measured by using the functional relationship in the step 1 as a mapping function so as to form a finite element load distribution model of the airfoil surface to be measured. Compared with prior art, the method for processing airfoil surface load of the invention considers the comparison between total load and total moment before and after load processing, and considers the comparison between a pressure distribution pattern and a finite element node load distribution pattern so that a designer could obviously judge the rationality of aerodynamic load process.

Description

Technical field [0001] The invention relates to the technical field of aircraft, in particular to a wing surface load processing method. Background technique [0002] The processing of aerodynamic loads must consider the comparison of the total load and the total moment before and after the load processing, as well as the comparison of the CP (pressure) distribution pattern and the finite element node load distribution pattern. In the process of aerodynamic load processing, the problem that needs to be solved is how to use the function of three-dimensional graphic display to visually compare and analyze the CP distribution and the finite element node force distribution. [0003] In the prior art, the total load and the total moment before and after load processing are usually compared, and the error after processing is controlled at 5%, and corrections are made if it exceeds 5%, ignoring the load distribution shape, which has certain limitations. [0004] Therefore, it is desirable ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 李军贵赵占文陈军
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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