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An experimental study on dynamic ice accretion process over the surfaces of rotating aero-engine spinners
An experimental study was conducted to investigate the dynamic ice accretion process over
the surfaces of rotating aero-engine spinners and to examine the detriment effects of the ice …
the surfaces of rotating aero-engine spinners and to examine the detriment effects of the ice …
Experimental investigation of the icing scaling test method for a rotating cone
F Zhang, L Zhang, Y Li, Z Liu… - Proceedings of the …, 2019 - journals.sagepub.com
One of the reliable methods of studying engine icing is to carry out testing in an icing wind
tunnel. Due to the operational limitations of test facility, model-size scaling is adopted. An …
tunnel. Due to the operational limitations of test facility, model-size scaling is adopted. An …
An Experimental Study of the Dynamic Ice Accreting Process over a Rotating Aero-engine Fan Model
I. Introduction accretion on the commercial aero-engines (ie, turbofans) is a topic of great
concern for aircraft operation safety near the area with super-cooled water droplets in the …
concern for aircraft operation safety near the area with super-cooled water droplets in the …
民用涡轴发动机进气系统结冰试验
宋建宇, 吴晶峰, 邱长波 - 航空动力学报, 2020 - jasp.com.cn
围绕**民航规章CCAR-33 部R2 版中第33.68 条款适航要求, 针对涡轴发动机提出了一种满足
适航要求的试验方法, 包括结冰关键点分析, 结冰取证试验点选定, 整机结冰取证试验三部分 …
适航要求的试验方法, 包括结冰关键点分析, 结冰取证试验点选定, 整机结冰取证试验三部分 …
[HTML][HTML] 吹气式旋转帽罩防冰特性
高艳欣, 周建军, **云单, 陆海鹰 - 南京航空航天大学学报, 2016 - jnuaa.nuaa.edu.cn
为研究吹气式旋转帽罩防冰特性, 采用三维模拟技术对其进行数值分析, 从流场,
水撞击和积冰特性3 个方面分析了吹气式旋转帽罩的防冰机理和效果, 并利用防冰试验器开展了 …
水撞击和积冰特性3 个方面分析了吹气式旋转帽罩的防冰机理和效果, 并利用防冰试验器开展了 …
旋转部件复杂表面水滴撞击计算
申晓斌, 张志**, 林贵**, 穆作栋, 卜雪琴 - 空气动力学学报, 2016 - kqdlxxb.xml-journal.net
为模拟旋转体结冰问题的过冷水滴运动及撞击过程, 基于欧拉方法及单旋转坐标系模型,
建立了三维旋转水滴运动模型, 并提出了相应的数值求解方法. 采用单旋转坐标系对空气及水滴 …
建立了三维旋转水滴运动模型, 并提出了相应的数值求解方法. 采用单旋转坐标系对空气及水滴 …
旋转帽罩结冰相似准则的冰风洞试验研究
张丽芬, 葛鑫, 张斐, 刘振侠, 马栋, 吕维进 - 实验流体力学, 2021 - syltlx.com
为了验证旋转帽罩冰风洞试验相似准则的适用性, 开展了旋转帽罩表面结冰过程研究,
推导了旋转帽罩结冰相似准则. 采用底面直径100 mm, 锥角80 的旋转锥作为原尺寸模型 …
推导了旋转帽罩结冰相似准则. 采用底面直径100 mm, 锥角80 的旋转锥作为原尺寸模型 …
涡扇发动机短舱结冰试验相似方法
杨倩, 董威, 郭之**, 郑梅 - 航空动力学报, 2019 - jasp.com.cn
通过分析短舱表面结冰缩比试验相似要求, 在保证绕流流场, 水滴撞击特性和结冰冰型相似的
基础上, 分别采用基于气流雷诺数, 气流韦伯数和水滴韦伯数3 种速度选取方法建立了试验相似 …
基础上, 分别采用基于气流雷诺数, 气流韦伯数和水滴韦伯数3 种速度选取方法建立了试验相似 …
Experimental investigations on ice accretion process and anti-/de-icing technology for aero-engine icing mitigation
L Li - 2018 - search.proquest.com
Aero-engine icing is widely recognized as a significant hazard to aviation safety in cold
weather. During flights, upon the im**ement of small, super-cooled, airborne water …
weather. During flights, upon the im**ement of small, super-cooled, airborne water …
Numerical Simulation of Ice Shedding From a Spinning Cone by Using Coupled CZM and XFEM
L Fu, Y Chen, M Xu, X Wu… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
In turbofan engine, ice accretion on spinning cone may lead to a decline in the engine
aerodynamic performance and an increase of the vibration amplitude of the engine. An …
aerodynamic performance and an increase of the vibration amplitude of the engine. An …