Image acquisition method for measuring pulsating pressure and noise of cavity model

An image acquisition and pulsating pressure technology, applied in the field of wind tunnel optical measurement and testing, can solve the problems of increasing model design and processing costs, difficult installation of pulsating pressure sensors, and low spatial resolution.

Pending Publication Date: 2022-02-18
INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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Problems solved by technology

[0005] However, in the above process, although the measurement accuracy of the pulsation pressure sensor is high, there are still many defects: ①Because the pulsation sensor protrudes or is recessed on the inner surface of the cavity, it will interfere with the flow field of the cavity, resulting in pulsation pressure and noise The measurement is inaccurate, so the sensor is required to be strictly flush with the surface of the cavity model, which makes the installation of the pulsation pressure sensor more difficult
②Installing the pulsating pressure sensor requires drilling and slotting the cavity model at the installation location and wiring channel, which increases the difficulty of model design and processing, and increases the cost of model design and processing
③The pulsating pressure sensor can only measure several points on the surface of the cavity, and the spatial resolution is very low, so it cannot meet the requirements of global surface measurement, and cannot obtain the acoustic characteristics and flow field structure details of the global cavity

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  • Image acquisition method for measuring pulsating pressure and noise of cavity model
  • Image acquisition method for measuring pulsating pressure and noise of cavity model

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Embodiment Construction

[0037] The technical solutions in the embodiments of the present application will be described below with reference to the drawings in the embodiments of the present application.

[0038] It should be noted that like numerals and letters denote similar items in the following figures, therefore, once an item is defined in one figure, it does not require further definition and explanation in subsequent figures. Meanwhile, in the description of the present application, relative terms such as "first", "second", etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply that these entities or operations, any such actual relationship or order exists. Moreover, the term "comprising" or any other variation thereof is intended to cover a non-exclusive inclusion such that a process, method, article or apparatus comprising a set of elements includes not only those elements but also other elements not expressly liste...

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Abstract

The invention discloses an image acquisition method for measuring pulsating pressure and noise of a cavity model. The method measures and calculates the pulsating pressure and noise of the cavity model based on a fast response pressure-sensitive paint technology and an image processing technology, and does not need a sensor for measurement, so that the installation of the sensor on the cavity model can be avoided, and thus, the design difficulty and the processing difficulty of the cavity model can be simplified, and the design cost and the processing cost of a model are reduced. In addition, surface measurement of a cavity surface area can be carried out, the spatial resolution is high, and global cavity pulsating pressure and noise data spectra can be obtained.

Description

technical field [0001] The application belongs to the technical field of wind tunnel optical measurement experiments, and in particular relates to an image acquisition method for measuring pulsating pressure and noise of a cavity model. Background technique [0002] Cavity structures are widely used in various fields. For example, in the field of aerospace, the embedded weapon compartment of fighter jets, the landing gear compartment of airliners, and the concave cavity for stabilizing flames in the combustion chamber of scramjet engines all involve cavity structure. [0003] Among them, the aerodynamic problem caused by the unsteady flow of the cavity is a very complex aerodynamic phenomenon, which is likely to cause failures in advanced aircraft using cavity structures in the aerospace field. Therefore, it is necessary to analyze the pulsating pressure and Noise is measured to better study cavities to ensure the safety of advanced aircraft. [0004] In the prior art, the...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/06G01M9/08
CPCG01M9/06G01M9/08Y02T90/00
Inventor 刘祥熊健王红彪黄辉刘大伟周方奇陈植
Owner INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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