Method for predicting gap between model tail cavity and supporting rod for wind tunnel test

A prediction method and model technology, applied in the field of experimental fluid mechanics, can solve the problems of unavailable collision prediction, unpredictability, and no real effect, etc., and achieve the effect of convenient implementation, improvement of experimental accuracy and efficiency, and saving experimental resources

Pending Publication Date: 2020-06-05
成都陆面体科技有限公司
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Problems solved by technology

The above two methods are mainly used to confirm and verify whether the model and the strut have collided in the wind tunnel test, and both have post facto nature, that is, it can be reflected only after the collision has occurred, and cannot be used for collision prediction, and cannot be used before the experiment starts. Predicting whether a collision will occur has no real effect on improving the accuracy of the experiment, improving the efficiency of the experiment, and saving experimental resources

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  • Method for predicting gap between model tail cavity and supporting rod for wind tunnel test
  • Method for predicting gap between model tail cavity and supporting rod for wind tunnel test
  • Method for predicting gap between model tail cavity and supporting rod for wind tunnel test

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Embodiment Construction

[0014] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below. Those who do not indicate the specific conditions in the examples are carried out according to the conventional conditions or the conditions suggested by the manufacturer.

[0015] The method for predicting the gap between the model tail cavity and the strut used in the wind tunnel test provided by the embodiment of the present invention will be described in detail below.

[0016] The embodiment of the present invention provides a method for predicting the gap between the model tail cavity and the strut for wind tunnel tests, which includes: using the difference between the physical data and the characteristic data to characterize the gap between the model tail cavity and the strut gap.

[0017] can be combined figure 1 , the physical dat...

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Abstract

The invention discloses a prediction method for a gap between a model tail cavity and a supporting rod for a wind tunnel test, and relates to the field of experimental fluid mechanics. The method comprises the step of representing a gap between the model tail cavity and the supporting rod by utilizing a difference value of physical data and characteristic data. The physical data comprises a modeltail cavity radius and a supporting rod radius, and the two radiuses are in a difference relation. The characteristic data comprises deflection angle data, model tail cavity supporting rod displacement and supporting rod head displacement, and the deflection angle data and the model tail cavity supporting rod displacement are summed and subtracted from the supporting rod head displacement to obtain an absolute value. The deflection angle data comprises the distance between the model tail cavity and the supporting rod head and the sine value of the model deflection angle, and the two are in a product relation. The method is simple, easy to use and convenient to implement, and can predict the collision between the model and the support rod before an experiment is carried out, and the methodfacilitates improving experiment planning, improving experiment accuracy and experiment efficiency and saving experiment resources.

Description

technical field [0001] The invention relates to the field of experimental fluid mechanics, in particular to a method for predicting the gap between a model tail chamber and a strut used in a wind tunnel test. Background technique [0002] At present, two methods are usually used to judge whether the tail cavity of the model collides with the strut. The first is to determine whether a collision has occurred by analyzing whether there is an abnormal change in the aerodynamic curve. The second is to judge whether a collision has occurred by painting the dye on the pole before the test and observing whether there are collision marks left on the place where the dye is applied. The above two methods are mainly used to confirm and verify whether the model and the strut have collided in the wind tunnel test, and both have post facto nature, that is, it can be reflected only after the collision has occurred, and cannot be used for collision prediction, and cannot be used before the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/28G06F119/14G01M9/02
CPCG01M9/02
Inventor 刘云楚
Owner 成都陆面体科技有限公司
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