1 |
INGELMAN-SUNDBERG M, TRUNOV O K, IVANIKO A. Methods for prediction of the influence of ice on aircraft flying characteristics[R]. Swedish-Soviet Working Group on Flight Safety, 1977.
|
2 |
KHODADOUST A, DOMINIK C, SHIN J, et al. Effect of In-flight ice accretion on the performance of a multi-element airfoil[R]. Montreal: International Icing Symposium, 1995.
|
3 |
IULIANO E, BRANDI V, MINGIONE G, et al. Water impingement prediction on multi-element airfoils by means of eulerian and Lagrangian approach with viscous and inviscid air flow[C]∥ 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2006.
|
4 |
YU C X, KE P, YU G F, et al. Investigation of water impingement on a multi-element high-lift airfoil by Lagrangian and Eulerian approach[J]. Propulsion and Power Research, 2015, 4(3): 161-168.
|
5 |
任靖豪, 王强, 刘宇, 等. 大型商用运输机机翼增升构型水滴撞击特性计算[J]. 空气动力学学报, 2021, 39(1): 52-58, 72.
|
|
REN J H, WANG Q, LIU Y, et al. Numerical simulation of droplet impingement characteristics on a high-lift configuration of a large commercial transport aircraft[J]. Acta Aerodynamica Sinica, 2021, 39(1): 52-58, 72 (in Chinese).
|
6 |
PETROSINO F, MINGIONE G, CAROZZA A, et al. Ice accretion model on multi-element airfoil[J]. Journal of Aircraft, 2011, 48(6): 1913-1920.
|
7 |
ÖZGEN S, CANıBEK M. Ice accretion simulation on multi-element airfoils using extended Messinger model[J]. Heat and Mass Transfer, 2009, 45(3): 305-322.
|
8 |
SANG W M, LI F W, SHI Y Y. Icing effect study for wing/body and high-lift wing configurations[C]∥ 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2007.
|
9 |
张恒, 李杰, 龚志斌. 多段翼型缝翼前缘结冰大迎角分离流动数值模拟[J]. 航空学报, 2017, 38(2): 520746.
|
|
ZHANG H, LI J, GONG Z B. Numerical simulation of separated flow around a multi-element airfoil at high angle of attack with iced slat[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(2): 520746 (in Chinese).
|
10 |
李冬, 张辰, 王福新, 等. 多段翼型的大粒径过冷水滴结冰特征及气动影响分析[J]. 上海交通大学学报, 2017, 51(8): 921-931.
|
|
LI D, ZHANG C, WANG F X, et al. An investigation on the characteristics of supercooled large droplet icing accretions and aerodynamic effects on high-lift configuration[J]. Journal of Shanghai Jiao Tong University, 2017, 51(8): 921-931 (in Chinese).
|
11 |
PRINCE RAJ L, LEE J W, MYONG R S. Ice accretion and aerodynamic effects on a multi-element airfoil under SLD icing conditions[J]. Aerospace Science and Technology, 2019, 85: 320-333.
|
12 |
MESSINGER B L. Equilibrium temperature of an unheated icing surface as a function of air speed[J]. Journal of the Aeronautical Sciences, 1953, 20(1): 29-42.
|
13 |
陈坚强, 吴晓军, 张健, 等. FlowStar: 国家数值风洞(NNW)工程非结构通用CFD软件[J]. 航空学报, 2021, 42(9): 625739.
|
|
CHEN J Q, WU X J, ZHANG J, et al. FlowStar: general unstructured-grid CFD software for National Numerical Windtunnel(NNW) Project[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(9): 625739 (in Chinese).
|
14 |
OZCER I, SWITCHENKO D, BARUZZI G S, et al. Multi-shot icing simulations with automatic re-meshing[C]∥ International Conference on Icing of Aircraft, Engines, and Structures. Warrendale: SAE International, 2019: 2019-01-1956.
|
15 |
SHIN J, BOND T H. Experimental and computational ice shapes and resulting drag increase for a NACA 0012 airfoil[C]∥ 5th Symposium on Numerical and Physical Aspects of Aerodynamic Flows. Washington, D. C.: NACA, 1992:19920019431.
|
16 |
MYERS T G. Extension to the messinger model for aircraft icing[J]. AIAA Journal, 2001, 39(2): 211-218.
|
17 |
MYERS T G, CHARPIN J P F, THOMPSON C P. Slowly accreting ice due to supercooled water impacting on a cold surface[J]. Physics of Fluids, 2002, 14(1): 240-256.
|
18 |
HILL J M. One-dimensional stefan problems: an introduction[M]. London: Longman Scientific & Technical, 1987
|
19 |
MARUYAMA D, BAILLY D, CARRIER G. High-quality mesh deformation using quaternions for orthogonality preservation[J]. AIAA Journal, 2014, 52(12): 2712-2729.
|
20 |
JIAO X M. Face offsetting: A unified approach for explicit moving interfaces[J]. Journal of Computational Physics, 2007, 220(2): 612-625.
|
21 |
PAPADAKIS M. Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet[R]. Washington, D. C.:NASA, 2002.
|