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基于沿程冷却法的冰晶沿程参数变化模拟

齐海峰 常士楠 任战鹏 杨映麟

航空学报2026,Vol.47Issue(4):1-13,13.
航空学报2026,Vol.47Issue(4):1-13,13.DOI:10.7527/S1000-6893.2025.32227

基于沿程冷却法的冰晶沿程参数变化模拟

Simulation of ice crystal parameters along path change based on path cooling method

齐海峰 1常士楠 1任战鹏 2杨映麟1

作者信息

  • 1. 北京航空航天大学 航空科学与工程学院,北京 100191
  • 2. 中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065
  • 折叠

摘要

Abstract

In order to solve the technical problems of ice crystal formation,the process of water droplet phase turning into ice crystals was numerically simulated by the path cooling method to determine the specific location and range of ice crystal formation,that is,the test section range for conducting the ice crystal icing simulation test.In the process of moving with the air flow,the ice crystal will have heat/mass transfer with the surrounding air,and its parameters such as diameter,temperature and velocity change significantly.Based on the path cooling method and phase transition cri-teria,the variation of ice crystal parameters under different conditions is studied.The results show that when the inlet wind speed of the stable section increases,the wind speed inside the test section increases significantly.Under the conditions of inlet wind speed of 10,15,20 m/s,the icing proportion inside the test section is relatively high,reaching more than 90%.At ambient temperatures of 233.15 K and 223.15 K,the water droplets have completely frozen into ice crystals near x=2.3 m.Furthermore,with the increase of the diameter of the water drop,the total water content in different sections along the test section gradually decreases,and the position where the water drops begins to freeze increases along the direction of movement.

关键词

水滴冻结/沿程冷却法/冰风洞/传热传质/冰晶生成

Key words

water droplet icing/path cooling method/ice wind tunnel/heat and mass transfer/ice crystal formation

分类

航空航天

引用本文复制引用

齐海峰,常士楠,任战鹏,杨映麟..基于沿程冷却法的冰晶沿程参数变化模拟[J].航空学报,2026,47(4):1-13,13.

基金项目

国家自然科学基金(12172031) (12172031)

强度与结构完整性国家重点实验室开放基金(LSSIKFJJ202405002)National Natural Science Foundation of China(12172031) (LSSIKFJJ202405002)

National Key Laboratory of Strength and Structural Integrity Open Fund(LSSIKFJJ202405002) (LSSIKFJJ202405002)

航空学报

1000-6893

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