DOI QR코드

DOI QR Code

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)
  • 투고 : 2017.01.16
  • 심사 : 2017.05.28
  • 발행 : 2017.06.30

초록

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.

키워드

참고문헌

  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
  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
  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
  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
  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
  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
  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
  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
  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
  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
  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
  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
  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
  17. 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
  18. 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
  19. 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
  20. 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
  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
  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
  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. 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
  27. 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