CN113392601A - Geometric feature analysis method of hydrodynamic noise line spectrum of cylinder-like shell - Google Patents

Geometric feature analysis method of hydrodynamic noise line spectrum of cylinder-like shell Download PDF

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CN113392601A
CN113392601A CN202110782864.3A CN202110782864A CN113392601A CN 113392601 A CN113392601 A CN 113392601A CN 202110782864 A CN202110782864 A CN 202110782864A CN 113392601 A CN113392601 A CN 113392601A
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line spectrum
cylinder
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hydrodynamic
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曹红丽
王晓燕
姚帅
方世良
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Southeast University
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Abstract

The invention discloses a geometric characteristic analysis method of a hydrodynamic noise line spectrum of a cylinder-like shell, which comprises the following steps: partitioning the CFD mesh and the mesh of the shell finite element surface by using Gambit software; acquiring wall surface pressure pulsation data, namely a cgns format file; importing grids of the shell finite element surface divided by Gambit into ICEM for grid data format conversion; importing the grid format. bdf file into Nastran to carry out shell material attribute, and calculating a free mode to obtain a.op 2 format file; setting a numerical model of hydrodynamic radiation noise; setting a boundary layer type; and establishing a data recovery surface, arranging a sensor on the data recovery surface, and solving a sound pressure frequency response diagram at the position of the sensor. The characteristic analysis method of the method utilizes a numerical method to solve, and can obtain the relevance between the length size of the cylinder-like shell and the line spectrum frequency.

Description

Geometric feature analysis method of hydrodynamic noise line spectrum of cylinder-like shell
Technical Field
The invention belongs to the technical field of signal processing, and particularly relates to a geometric characteristic analysis method of a hydrodynamic noise line spectrum of a cylinder-like shell.
Background
When the cylinder-like shell passes through a water medium, a turbulent boundary layer is formed on the surface of the cylinder-like shell, unstable flow is blocked by the surface of the shell, momentum fluctuation near the wall surface is balanced by pressure fluctuation on the interface, and the pressure fluctuation of the boundary layer is used as a random excitation source to be excited to form hydrodynamic noise. The hydrodynamic noise is caused by disturbance in a boundary layer of surrounding turbulence generated when the cylindrical shell passes through a water medium, pulsating pressure on a wall surface and structural vibration caused by coupling action of fluid and solid. In general, hydrodynamic noise is of a much lower magnitude than mechanical and propeller noise, but as the speed of motion increases, the proportion of hydrodynamic noise in the total noise increases.
At present, the numerical calculation method of hydrodynamic noise mainly comprises three methods, namely a theoretical analysis method, a numerical prediction method and an experimental method. The theoretical analysis method has a strict mathematical and physical derivation formula, but is only limited to a shell model with a simple geometric shape, the actual model needs to be simplified, and the theoretical method is limited when the actual engineering problem is processed.
Disclosure of Invention
The purpose of the invention is as follows: aiming at the problems and the defects of the existing method, the invention provides the geometric characteristic analysis method of the hydrodynamic noise line spectrum of the cylindrical shell, the numerical prediction has certain adaptability to the hydrodynamic noise problem with complex structure and boundary, and the engineering practicability is strong.
The technical scheme is as follows: in order to achieve the purpose, the invention adopts the following technical scheme: a geometric characteristic analysis method of a hydrodynamic noise line spectrum of a cylinder-like shell comprises the following steps:
step 1, dividing CFD grids and grids on a shell finite element surface by using Gambit software;
step 2, performing steady-state flow field calculation in the Fluent, and then performing unsteady-state calculation to obtain wall surface pressure pulsation data, namely a cgns format file;
step 3, importing grids on the shell finite element surface divided by Gambit into ICEM for grid data format conversion, and converting into bdf format;
step 4, importing the grid format. bdf into Nastran to set the attribute of the shell material, and calculating to obtain a free mode.op 2 format file; the material property setting is steel, meaning the material property setting is steel.
Step 5, importing the free steady state of Nastran, op2 format file and the shell wall surface pressure fluctuating pressure data exported by Fluent into VA ONE software, and setting a numerical model of hydrodynamic radiation noise;
step 6, adding turbulent boundary layer load to the surface of the finite element model of the cylinder-like shell, and setting the type of the boundary layer;
step 7, establishing a data recovery surface which is a spherical data recovery surface at the center of the propeller and is set as a boundary meta-model; arranging a sensor on a data recovery surface, and solving a hydrodynamic noise sound pressure frequency response diagram at the position of the sensor by adopting VA ONE software;
and 8, analyzing the hydrodynamic noise sound pressure frequency response line spectrum characteristics of the similar cylindrical shells with different length sizes, so as to obtain the relation between the length size of the similar cylindrical shell and the hydrodynamic noise sound pressure frequency response line spectrum.
Has the advantages that: compared with the prior art, the method has the following beneficial effects:
(1) the estimation method solves hydrodynamic noise in VA ONE software, quickly solves the relation between the length size of the similar cylindrical shell and the hydrodynamic noise line spectrum, and has strong engineering practicability;
(2) the estimation method can solve the problem of hydrodynamic noise line spectrum characteristic analysis with complex structure and boundary;
drawings
FIG. 1 is a schematic flow diagram of the process of the present invention;
FIG. 2 is a diagram of a numerical model of a cylinder-like shell;
FIG. 3 is a spatial distribution map of test points;
FIG. 4 is a graph of hydrodynamic noise sound pressure frequency response of a cylinder-like housing;
FIG. 5 is a graph of the acoustic pressure frequency response of hydrodynamic noise of cylindrical shells of different lengths;
FIG. 5(a) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 5 m;
FIG. 5(b) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 5.5 m;
FIG. 5(c) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 5.98533 m;
FIG. 5(d) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 6.5 m;
FIG. 5(e) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 7 m;
FIG. 5(f) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 7.5 m;
FIG. 5(g) is a graph of the acoustic pressure frequency response of hydrodynamic noise at a cylinder-like housing length of 7.8 m;
fig. 5(h) is a sound pressure frequency response graph of hydrodynamic noise at a cylinder-like housing length of 8.2 m.
Detailed Description
The invention is further described with reference to the following figures and examples:
as shown in fig. 1, the method for analyzing geometrical characteristics of hydrodynamic noise line spectrum of a cylindrical shell of the present invention includes the following steps:
(1) the size parameters of the cylinder-like shell are respectively set as: the thickness h of the cylinder-like shell is 0.027m, the radius r is 0.533m, the length L of the circular platform part at the front end is 0.2132m, the length L of the cylinder-like shell is 4.867883m, an experimental paddle T1 is used as a propeller, the diameter is 0.2482m, and four-blade large-side inclined paddles are arranged. Partitioning a CFD computational grid and a grid of a shell finite element surface by using Gambit software;
(2) performing steady-state flow field calculation in the Fluent, then performing unsteady-state flow field calculation, wherein the iteration step length of the unsteady-state calculation is 0.000462963s, the environmental pressure is 113kPa, the rotating speed is 30r/s, and wall surface pressure pulsation data is derived;
(3) importing grids of the shell finite element surface divided by Gambit into ICEM for grid data format conversion, and converting into bdf format;
(4) introducing the grid format bdf into Nastran for shell material property setting, wherein the shell material property is steel, and the density rho of the cylindrical shell isp7800kg/m3, the poisson ratio sigma is 0.3, the young modulus E is 2.1 × 1011, and a free mode file op2 format is obtained through calculation;
(5) importing a Nastran free steady state op2 format file and Fluent exported shell wall surface pressure fluctuating pressure data, and importing a cgns format file into VA ONE software to set a numerical model of hydrodynamic radiation noise;
(6) adding turbulent boundary layer load to the surface of finite element model of cylinder-like shell, sound velocity C in water01500m/s, sea water density ρ0Setting a turbulent boundary layer type as 1000kg/m 3;
(7) establishing a data recovery surface, setting the data recovery surface as a boundary meta-model, arranging sensors on the data recovery surface, establishing a spherical data recovery surface with the length of 2.5m by taking the center of a propeller as an original point, and arranging 8 sensors on the data recovery surface as a device for receiving hydrodynamic noise of a cylindrical shell of a hydrophone test type, wherein the numerical calculation model and the spatial distribution diagram of the test points are shown in fig. 2 and 3. With the above arrangement, the VA ONE software solves the sound pressure frequency response plot at the sensor location, as shown in fig. 4.
(8) And analyzing the sound pressure frequency response line spectrum characteristics of the hydrodynamic noise of the cylinder-like shells with different length and size.
Setting the length parameters of the cylinder-like shell to be 5m, 5.5m, 5.98533m, 6.5m, 7.0m, 7.5m, 7.8m and 8.2m respectively, obtaining the sound pressure frequency responses of the 8 sensor positions corresponding to the length parameters of the different cylinder-like shells according to the steps 1-7, finding the strongest line spectrum frequency in the sound pressure frequency response diagram of the different length parameters as shown in the figures 5(a) -5(h) in sequence, and as shown in the table 1, reducing the frequency of the corresponding line spectrum along with the increase of the length of the line spectrum.
TABLE 1 hydrodynamic noise line spectrum distribution corresponding to different cylinder shell lengths
Figure BDA0003157800610000031
Figure BDA0003157800610000041

Claims (4)

1. A geometric feature analysis method of a hydrodynamic noise line spectrum of a cylinder-like shell is characterized by comprising the following steps:
step 1, dividing CFD grids and grids on a shell finite element surface by using Gambit software;
step 2, performing unsteady calculation in Fluent to obtain wall surface pressure pulsation data, namely a cgns format file;
step 3, importing grids on the shell finite element surface divided by Gambit into ICEM for grid data format conversion, and converting into bdf format;
step 4, importing the grid data format of bdf into Nastran to set the shell material attribute, and calculating to obtain a free mode file of op2 format;
step 5, importing the free steady state of Nastran, op2 format file and the shell wall surface pressure fluctuating pressure data exported by Fluent into VA ONE software, and setting a numerical model of hydrodynamic radiation noise;
step 6, adding turbulent boundary layer load to the surface of the finite element model of the cylinder-like shell, and setting the type of the boundary layer;
step 7, establishing a data recovery surface, setting the data recovery surface as a boundary element model, arranging a sensor on the data recovery surface, and solving a hydrodynamic noise sound pressure frequency response diagram at the position of the sensor by adopting VA ONE software;
and 8, analyzing the hydrodynamic noise sound pressure frequency response line spectrum characteristics of the similar cylindrical shells with different length sizes, so as to obtain the relation between the length size of the similar cylindrical shell and the hydrodynamic noise sound pressure frequency response line spectrum.
2. The method for analyzing the geometric characteristics of the hydrodynamic noise line spectrum of the cylindrical shell according to claim 1, wherein in the step 2, steady-state flow field calculation is performed in Fluent, and then unsteady-state flow field calculation is performed to obtain wall surface pressure pulsation data.
3. The method for geometrical feature analysis of hydrodynamic noise line spectrum of cylindrical hull according to claim 1, wherein in step 4, the material property is set to steel.
4. The method of claim 1, wherein in step 7, the data recovery surface is a spherical data recovery surface centered on the propeller.
CN202110782864.3A 2021-07-12 2021-07-12 Geometric feature analysis method of hydrodynamic noise line spectrum of cylinder-like shell Pending CN113392601A (en)

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