Browse > Article
http://dx.doi.org/10.5139/IJASS.2017.18.2.352

3D Numerical Simulation of Ice Accretion on a Rotating Surface  

Mu, Zuodong (Laboratory of Fundamental Science on Ergonomics and Environmental Control, School of Aeronautic Science and Engineering, Beihang University)
Lin, Guiping (Laboratory of Fundamental Science on Ergonomics and Environmental Control, School of Aeronautic Science and Engineering, Beihang University)
Bai, Lizhan (Laboratory of Fundamental Science on Ergonomics and Environmental Control, School of Aeronautic Science and Engineering, Beihang University)
Shen, Xiaobin (Laboratory of Fundamental Science on Ergonomics and Environmental Control, School of Aeronautic Science and Engineering, Beihang University)
Bu, Xueqin (Laboratory of Fundamental Science on Ergonomics and Environmental Control, School of Aeronautic Science and Engineering, Beihang University)
Publication Information
International Journal of Aeronautical and Space Sciences / v.18, no.2, 2017 , pp. 352-364 More about this Journal
Abstract
A novel 3D mathematical model for water film runback and icing on a rotating surface is established in this work, where both inertial forces caused by the rotation and shear forces due to the air flow are taken into account. The mathematical model of the water film runback and energy conservation of phase transition process is established, with a cyclical average method applied to simulate the unsteady parameters variation at angles of attack. Ice accretion on a conical spinner surface is simulated and the results are compared with the experimental data to validate the presented model. Then Ice accretion on a cowling surface is numerically investigated. Results show that a higher temperature would correspond to a larger runback ice area and thinner ice layer for glaze ice. Rotation would enhance the icing process, while it would not significantly affect the droplet collection efficiency for an axi-symmetric surface. In the case at angle of attack, the effect of rotation on ice shape is appreciable, ice would present a symmetric shape, while in a stationary case the shape is asymmetric.
Keywords
Aircraft icing; Water film runback; Numerical simulation; Rotating;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Anderson, J, D., Fundamentals of aerodynamics, McGraw-Hill, Massachusetts, 2001.
2 Al-Khalil, K. M., Keith, T. G. and De Witt, K. J. "Icing Calculations on a Typical Commercial Jet Engine Inlet Nacelle", Journal of aircraft, Vol. 34, No. 1, 1997, pp. 87-93. DOI: 10.2514/2.2139   DOI
3 Mason, J. G., Strapp, W. and Chow, P., "The Ice Particle Threat to Engines in Flight", 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2006-206, Reno, Nevada. 2006. DOI: 10.2514/6.2006-206   DOI
4 Ruff, G. A. and Berkowitz, B. M., Users' manual for the NASA Lewis ice accretion prediction code (LEWICE), 1990.
5 Hedde, T. and Guffond, D., "ONERA Three-Dimensional Icing Model", AIAA journal, Vol. 33, No. 6, 1995, pp. 1038- 1045. DOI: 10.2514/3.12795   DOI
6 Gent, R. W., "TRAJICE2 - A Combined Water Droplet Trajectory and Ice Accretion Prediction Program for Aero Foils", Royal Aerospace Establishment, Farnborough, Hampshire, 1990.
7 Franc-para, Morency, O., Tezok, F. and Paraschivoiu, I., "Anti-Icing System Simulation Using CANICE", Journal of Aircraft, Vol. 36, No. 6, 1999, pp. 999-1006. DOI: 10.2514/2.2541   DOI
8 Messinger, B. L., "Equilibrium Temperature of an Unheated Icing Surface as a Function of Air Speed", Journal of the Aeronautical Sciences, Vol. 20, No. 1, 1953, pp. 29-42. DOI: 10.2514/8.2520   DOI
9 Myers, T. G., Charpin, J. P. F. and Thompson, C. P., "Slowly Accreting Ice due to Supercooled Water Impacting on a Cold Surface", Physics of Fluids (1994-present), Vol. 14, No. 1, 2002, pp. 240-256. DOI: 10.1063/1.1416186   DOI
10 Myers, T. G., "Extension to the Messinger Model for Aircraft Icing", AIAA Journal, Vol. 39, No. 2, 2001, pp. 211-218. DOI: 10.2514/2.1312   DOI
11 Li, X., Bai, J., Hua, J., Wang, K. and Zhang, Y., "A Spongy Icing Model for Aircraft Icing", Chinese Journal of Aeronautics, Vol. 27, No. 1, 2014, pp. 40-51. DOI: 10.1016/j.cja.2013.12.004   DOI
12 Shen, X., Lin, G., Yu, J. and Bu, X., "Three-Dimensional Numerical Simulation of Ice Accretion at the Engine Inlet", Journal of Aircraft, Vol. 50, No. 2, 2013, pp. 635-642. DOI: 10.2514/1.C031992   DOI
13 Beaugendre, H., Morency, F. and Habashi, W. G., "FENSAP-ICE's Three-Dimensional In-Flight Ice Accretion Module: ICE3D", Journal of Aircraft, Vol. 40, No. 2, 2003, pp. 239-247. DOI: 10.2514/2.3113   DOI
14 Baruzzi, G., Tran, P., Habashi, W. G. and Akel, I., "FENSAP-ICE: Progress Towards a Rotorcraft Full 3-D Icing Simulation System", AIAA-2003-0024, 2003. DOI: 10.2514/6.2003-24   DOI
15 Beaugendre, H., Morency, F. and Habashi, W. G., "Development of a Second Generation In-Flight Icing Simulation Code", Journal of Fluids Engineering, Vol.128, No.2, 2006, pp. 378-387. DOI: 10.1115/1.2169807   DOI
16 Thomas, R. and Habashi, W. G., "FENSAP-ICE Simulation of Icing on Wind Turbine Blades, Part 1: Performance Degradation", 51st AIAA Aerospace Sciences Meeting, Grapevine, Texas, 2013. DOI: 10.2514/6.2013-750   DOI
17 Chen, N., Ji, H., Hu, Y., Wang, J. and Cao, G., "Experimental Study of Icing Accretion on a Rotating Conical Spinner", Heat and Mass Transfer, Vol. 51, No. 12, 2015, pp. 1717-1729. DOI: 10.1007/s00231-015-1536-0   DOI
18 Thomas, R. and Habashi, W. G., "FENSAP-ICE Simulation of Icing on Wind Turbine Blades, Part 2: Ice Protection System Design", 51st AIAA Aerospace Sciences Meeting, Grapevine, Texas, 2013. DOI: 10.2514/6.2013-751   DOI
19 David, S. and Habashi, W. G., "FENSAP-ICE Simulation of Complex Wind Turbine Icing Events, and Comparison to Observed Performance Data", 32nd ASME Wind Energy Symposium, National Harbor, Maryland, 2014. DOI: 10.2514/6.2014-1399   DOI
20 Cristhian, N. A., Martin, S. A. and Habashi, W. G., "FENSAP-ICE-Unsteady: Unified In-Flight Icing Simulation Methodology for Aircraft, Rotorcraft, and Jet Engines", Journal of Aircraft, Vol.48, No.1, 2011, pp. 119-126. DOI: 10.2514/1.C000327   DOI
21 Belz, R., Brasier, C., Murphy, P. and Davis, T., "A Turbine Engine Inlet Viewing System", 22nd Joint Propulsion Conference, Huntsville, AL, 1986. DOI: 10.2514/6.1986-1647   DOI
22 Rothmayer, A. P. and Tsao, J. C., "Water Film Runback on an Airfoil Surface", 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 2000. DOI: 10.2514/6.2000-237   DOI
23 Newmerical Technologies Int, FENSAP-ICE, Software Package, Ver. 2011R1.0c, Canada, 2011.
24 Incropera, F. P. and Dewitt, D. P., Fundamentals of Heat and Mass Transfer. 5th ed. John Wiley & Sons, New York, 2002, pp. 357-361.
25 Yang, S., Lin, G. and Shen, X., "An Eulerian method for Water Droplet Impingement Prediction and its Implementations", Proceeding of the 1st International Symposium on Aircraft Airworthiness, Beijing, 2009.
26 Zhang, L., Zhang, M., Zhang, X. and Liu, Z., "Modeling of Ice Accretion on Rotating Cone in Aero-Engine", 52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, UT, 2016. DOI: 10.2514/6.2016-5059   DOI
27 Al-Khalil, K., Horvath, C., Miller, D., Wright, W., Al- Khalil, K., Horvath, C. and Wright, W., "Validation of NASA Thermal Ice Protection Computer Codes. III - The Validation of ANTICE", 35th AIAA Aerospace Sciences Meeting and Exhibit 1997, Reno, NV, 1997. DOI: 10.2514/6.1997-51   DOI