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Flight vehicle wind tunnel test data scripted-processing system and method

A wind tunnel test and scripting technology, applied in electrical digital data processing, special data processing applications, instruments, etc., can solve the problems of time-consuming and laborious wind tunnel data, long processing cycle, difficult use, etc., and achieve a simple and reliable implementation method. Fast processing, avoiding the effects of extraction and computation

Active Publication Date: 2018-02-23
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The above characteristics make wind tunnel data time-consuming and labor-intensive, making it difficult to use
[0004] The traditional wind tunnel test data processing is to copy the variables and data in the test file, and then process it through Excel software or self-written software, but the processing cycle is still long and error-prone

Method used

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  • Flight vehicle wind tunnel test data scripted-processing system and method

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Embodiment Construction

[0015] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0016] Such as figure 1 As shown, the aircraft wind tunnel test data script processing system of the present invention includes:

[0017] The train schedule editor, which has the functions of train schedule editing, expansion, merging and splicing, and also has the function of marking file parameters, such as the data file path and extension corresponding to the train number; through the train schedule editor, users can edit different The train schedule of the wind tunnel test is merged, spliced ...

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Abstract

The invention provides a flight vehicle wind tunnel test data scripted-processing system and method. The system comprises a cart number table editor having cart number table editing, extending, merging and splicing functions, a special script explanator for executing script explanation and obtaining a final data processing result, and a script editor mainly used for providing a script editing function easy for a user to use. An interface is provided for a script operating result through data postprocessing, and data display or sending is performed. By adopting the system and method, data extracting and operating functions based on cart number tables are achieved, and extraction and operation of original data of tunnel tests are avoided. Compared with a traditional processing method, the achievement method is simple, reliable, high in treating speed and good in script reusability.

Description

technical field [0001] The invention relates to a data script processing system and method, in particular to an aircraft wind tunnel test data script processing system and method. Background technique [0002] Studying and mastering the aerodynamic characteristics of aircraft is one of the basic tasks of aircraft design. In engineering practice, the mathematical description of the aerodynamic model is obtained through calculation through mathematical models and original data points, and then used by other professions to realize aircraft design. In addition to the mathematical model, the description of the aerodynamic characteristics of the aircraft needs corresponding original data. Judging from the current status, these raw data points are mainly obtained through wind tunnel tests. [0003] Aircraft wind tunnel test files have the following characteristics: 1. After the data is extracted from the wind tunnel test data file, it must be checked for legality, splicing, and s...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/15
Inventor 阮文华周志超郝莲英叶茂束川良孟万里
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG