Effects of ice accretions on aircraft aerodynamics
FT Lynch, A Khodadoust - Progress in Aerospace Sciences, 2001 - Elsevier
This article is a systematic and comprehensive review, correlation, and assessment of test
results available in the public domain which address the aerodynamic performance and …
results available in the public domain which address the aerodynamic performance and …
Experimental and computational simulation of in-flight icing phenomena
RJ Kind, MG Potapczuk, A Feo, C Golia… - Progress in Aerospace …, 1998 - Elsevier
This paper reviews experimental and computational methods used for simulation of ice
accretion on aircraft flying through icing conditions. Such methods were recently reviewed …
accretion on aircraft flying through icing conditions. Such methods were recently reviewed …
Impact of erosion testing aspects on current and future flight conditions
O Gohardani - Progress in Aerospace Sciences, 2011 - Elsevier
High speed of aero vehicles including commercial and military aircraft, missiles, unmanned
air vehicles, as well as conceptual aircraft of the future are imposing larger restrictions on the …
air vehicles, as well as conceptual aircraft of the future are imposing larger restrictions on the …
Numerical simulation of ice accretions on an aircraft wing
Y Cao, C Ma, Q Zhang, J Sheridan - Aerospace Science and Technology, 2012 - Elsevier
An approach based on the Eulerian two-phase flow theory to numerically simulate ice
accretions on an aircraft wing is developed. The air flowfield is obtained through Euler flow …
accretions on an aircraft wing is developed. The air flowfield is obtained through Euler flow …
Numerical simulation of rime ice on NREL Phase VI blade
L Hu, X Zhu, J Chen, X Shen, Z Du - Journal of Wind Engineering and …, 2018 - Elsevier
Wind turbine installation in cold regions is prone to icing events. In this study, rime ice on the
rotating NREL Phase VI blade is simulated. First, an icing model is developed and validated …
rotating NREL Phase VI blade is simulated. First, an icing model is developed and validated …
A three-dimensional aircraft ice accretion model based on the numerical solution of the unsteady Stefan problem
T Liu, K Qu, J Cai, S Pan - Aerospace Science and Technology, 2019 - Elsevier
This paper develops a three-dimensional aircraft ice accretion model based on the
numerical solution of the unsteady Stefan problem. In this model, for both rime and glaze ice …
numerical solution of the unsteady Stefan problem. In this model, for both rime and glaze ice …
[PDF][PDF] 结冰面水滴收集率欧拉计算方法研究及应用
易贤, 王开春, 桂业伟, 朱国林 - ACTA AERODYNAMICA …, 2010 - kqdlxxb.xml-journal.net
结冰面水滴收集率欧拉计算方法研究及应用 Page 1 第28卷第5期 空气动力学学报 V01.28.No.5
2010年10月 ACTA AERODYNAMICA SINICA Oct..2010 -I·—_·—·—_—___-————_—-·—··_——-_—·——_-_-·_—_-__-·-_·_·—-_—·—_—_————__—·_··—__—_—_——·_—_____________—·—·_—·—·_—-—__————_—·‘!■ …
2010年10月 ACTA AERODYNAMICA SINICA Oct..2010 -I·—_·—·—_—___-————_—-·—··_——-_—·——_-_-·_—_-__-·-_·_·—-_—·—_—_————__—·_··—__—_—_——·_—_____________—·—·_—·—·_—-—__————_—·‘!■ …
[HTML][HTML] 飞机热气防冰系统研究
常士楠, 杨波, 冷梦尧, 赵媛媛, 刘明阳 - 航空动力学报, 2017 - jasp.com.cn
介绍了飞机热气防冰系统的应用背景及基本结构, 回顾了其发展历程及国内外研究现状.
从防冰表面水滴撞击特性计算, 蒙皮外部结冰/溢流水模型建立, 热气防冰腔内部结构参数研究 …
从防冰表面水滴撞击特性计算, 蒙皮外部结冰/溢流水模型建立, 热气防冰腔内部结构参数研究 …
Development of a 3D Eulerian/Lagrangian aircraft icing simulation solver based on OpenFOAM
H Han, Z Yin, Y Ning, H Liu - Entropy, 2022 - mdpi.com
A 3D icing simulation code is developed in the open-source CFD toolbox OpenFOAM. A
hybrid Cartesian/body-fitted meshing method is used to generate high-quality meshes …
hybrid Cartesian/body-fitted meshing method is used to generate high-quality meshes …
3D ice accretion simulation for complex configuration basing on improved messinger model
CX Zhu, CL Zhu, B Fu - Advanced Materials Research, 2014 - Trans Tech Publ
Ice accretion on 3D complex configuration is studied by numerical methods. The flow field is
obtained by using Fluent 6.0 with a SA turbulence model. Droplet trajectories and …
obtained by using Fluent 6.0 with a SA turbulence model. Droplet trajectories and …