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Development and Validation of Aircraft Icing Computational Simulation Code

机译:飞机结冰计算仿真码的开发与验证

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The purpose of this paper is to present some results on the development and verification of NUAA-ICE2D icing software code, which contains five separate program modules and a graphical user interface. Computational simulation of the ice accretion process on airfoils using multiple time-steps is studied in this paper. Firstly, all the modular codes for icing computation have been established in FORTRAN90 based on the Dynamic Link Library (DLL), and then a software package to perform normal functions of these modules has been developed using Microsoft Foundation Classes (MFC) framework. In addition, this icing software has some visualization tools that can help user analyze, explore and understand the simulation data. The architecture of the software, the functions of each component, its application to icing prediction and the further development are also discussed in this document. It is shown that all the modular codes of the software have good precision and fast calculation velocity during the process of grid generation, flow field calculation, droplet impingement calculation and ice growth analysis because of use of DLL and MFC, the illustration chart of operational interface is briefly shown in Figure 1. This platform software not only has established a reliable data communications law among these computational modules, but also has given an efficient way to predict the ice-layer accretion on the surfaces of geometry, the results are compared we are in accordance with the experimental data, shown in Figure 2. Once the calculations for ice accretion are activated, the software can call the five modules alternately and automatically in a robust way. This paper will provide some new techniques for predicting the ice accretion on airfoil efficiently and developing integrated icing software using mixed-language programming, which can be used in the stage of airfoil design and assessment. This paper presents some new ideas to improve the efficiency and reliability in icing calculations, especially in user-oriented way.
机译:本文的目的是提供一些结果对NUAA-ICE2D结冰软件代码的开发和验证,其中包含五个单独的程序模块和图形用户界面。在本文中研究了使用多个时间步骤的翼型上的冰增射过程的计算模拟。首先,在Fortran90基于动态链接库(DLL)在Fortran90中建立了所有模块化代码,然后使用Microsoft Foundation类(MFC)框架开发了一种用于执行这些模块的正常功能的软件包。此外,此糖平软件还具有一些可视化工具,可以帮助用户分析,探索和理解模拟数据。本文档还讨论了软件的架构,每个组件的功能,其应用于结冰预测和进一步的开发。结果表明,由于使用DLL和MFC,所有模块化软件的所有模块码在网格生成过程中具有良好的精度和快速计算速度,流场计算,液滴冲击计算和冰增长分析,操作界面的图示简要介绍如图1所示。该平台软件不仅在这些计算模块中建立了可靠的数据通信定律,而且还给出了在几何形状表面上预测冰层吸收的有效方法,结果比较了结果按照实验数据,如图2所示。一旦激活了冰增冰的计算,软件可以以强大的方式交替呼叫五个模块。本文将提供一些新的技术来有效地预测翼型上的积冰,并使用混合语言编程,可在翼型设计和评估阶段使用集成开发软件结冰。本文介绍了一些新的想法,以提高结冰计算中的效率和可靠性,尤其是面向用户的方式。

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