Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Water plane wave water surface take-off and landing water-gas two-phase flow numerical simulation method

A numerical simulation and seaplane technology, applied in design optimization/simulation, CAD numerical modeling, electrical digital data processing, etc., can solve problems such as imperfect research work, achieve the effect of improving calculation efficiency and ensuring wave-making accuracy

Pending Publication Date: 2021-10-19
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF0 Cites 5 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the aircraft lands on the still water surface, the distance between the body and the free liquid surface only needs to adjust the horizontal position of the liquid surface. For wave landing, not only the balance position of the wave needs to be adjusted, but also the horizontal relative position between the wave and the body needs to be adjusted, namely The initial phase of the wave is required, and the research work in this area is not yet perfect, and it will also be the content that this patent will focus on

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Water plane wave water surface take-off and landing water-gas two-phase flow numerical simulation method
  • Water plane wave water surface take-off and landing water-gas two-phase flow numerical simulation method
  • Water plane wave water surface take-off and landing water-gas two-phase flow numerical simulation method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0040] The present invention will be further described below in conjunction with accompanying drawing.

[0041] In this embodiment, a seaplane regular wave landing is used as a demonstration, and the basic solution steps are shown in figure 1 .

[0042] In the first step, for the complex free liquid surface situation, the calculation domain grid adopts a multi-region and multi-level division strategy, and the cross-section shows the image 3 . Area I is a rectangular encryption area near the aircraft; area II is an aircraft head-on wave fan area; area III is an aircraft wake fan area; area IV is other areas.

[0043] Among them, the grid in area I has the highest level of grid encryption. Except for the boundary layer grid and the space grid with drastic changes in the physical quantity of the flow field, the other grid sizes in this area are specified according to the wave parameters. 80 grids are arranged, and 20 grids are arranged in a single wave height direction. Area...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention provides a water plane wave water surface take-off and landing water-gas two-phase flow numerical simulation method, which is based on an integral dynamic grid technology and a speed inlet wave making technology, and improves a grid division strategy and a flow field initialization method, thereby realizing unsteady flow field calculation of water plane wave water surface take-off and landing. In order to research the problem of wave dampening of a water surface aircraft, according to the method, an initial phase item and an initial balance position item are added in a wave surface equation, a wave velocity field and a pressure field function, so that phase deviation of waves in a computational domain along a propagation direction and vertical deviation of a wave balance position are realized; and therefore, the wave is in contact with the object in an extremely short solving time, and the time of waiting for the head wave by the object is saved. Compared with the conventional dynamic grid method, the method has the advantages that the grid quantity can be reduced, the grid utilization rate can be improved, and higher calculation speed can be obtained while the solving precision is ensured.

Description

technical field [0001] The invention relates to the field of aircraft take-off and landing tests, in particular to a numerical simulation method for water-air two-phase flow of a seaplane taking off and landing on a wave surface. Background technique [0002] Seaplanes are different from conventional aircraft. According to their mission requirements, they should have the ability to take off and land on the water, and be able to operate under certain sea conditions. Therefore, evaluating the take-off and landing capability of a seaplane on wave water is very important for flight safety. At present, the research methods for this problem are mainly divided into three methods: experimental research, theoretical calculation and numerical simulation. Experimental research requires a lot of laboratory construction costs, and the test data is often limited by equipment conditions, and the test results are relatively simple; theoretical calculations use empirical formulas to estimat...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/15G06F30/23G06F30/28G06F111/10G06F113/08G06F119/14
CPCG06F30/15G06F30/23G06F30/28G06F2111/10G06F2113/08G06F2119/14
Inventor 肖天航卢昱锦邓双厚支豪林朱震浩陆召严
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products