欧拉壁膜模型在结冰模拟中的扩展

doi:10.7527/S1000-6893.2023.29287

Abstract

Abstract:

In icing thermodynamic models， while the description of heat transfer and phase change is complete， the description of water film flow is usually simplified. To solve this problem， the calculation-correction method is used to expand the ability of Eulerian Wall Film （EWF） model in icing simulation， and the characteristics of the extended model in numerical schemes and icing prediction are studied. Calculations show that the icing rate gradually stabilizes over time. During the calculation， the second-order implicit method and the second-order upwind scheme show better stability， and the time-step and temporal/spatial differencing scheme have little effect on the calculation accuracy. In terms of icing prediction， the extended model has more advantages for the icing prediction of NACA0015 airfoil， compared with LEWICE software； the extended model is closer to the experimental results in the prediction of ice horn at relatively high speeds， compared with the icing model that simplifies the flow of the water film. In addition， the extended model also shows good adaptability in the icing simulation of the 30P30N airfoil and DPW aircraft.

Key words: aircraft icing, Eulerian wall film model, water film flow, data format, icing prediction

CLC Number:

V211.3

Huajie XIONG, Yijing AN, Zhulong WU, Zhihong ZHOU. Extension of Eulerian wall film model in icing simulation[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729287-729287.

Figures/Tables 11

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案例	速度/（m·s^-1）	攻角/（^o）	温度/K	LWC/（g·m^-3）	MVD/（10^-6 m）	结冰时间/s
401	102.80	3.50	265.37	0.55	20	420
425	67.10	3.50	244.51	1.00	20	360
421	67.10	3.50	268.40	1.00	20	360
422	67.10	3.50	266.74	1.00	20	360
402	102.80	3.50	263.71	0.55	20	420
624963	95.22	0	262.85	0.75	19	600
624965	95.22	0	262.85	0.50	25	600
1	102.80	8.00	262.04	0.86	20	270
2	142.73	0	262.04	1.50	20	270

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Extension of Eulerian wall film model in icing simulation

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