考虑侵蚀效应的冰晶/混合相结冰计算方法

doi:10.7527/S1000-6893.2023.28609

Abstract

Abstract:

The ingestion of ice crystals and icing inside the aero engine is a significant cause of aero engine damage and power loss. Researching on the calculation method for ice crystal/mixed phase icing， and systematically analyzing the physical model of ice crystal icing are among the major approaches to the study on the internal icing process of aero engines to ensure the safety of flight airworthiness. Focusing on the calculation of ice crystal/mixed phase icing， we establish， under the Lagrange framework， a complete numerical calculation method for ice crystal/mixed phase icing， covering multiple physical phenomena such as ice crystal motion-heat and mass transfer， ice crystal adhesion， mixed phase icing phase transition， and ice crystal erosion. The corresponding calculation program is then developed based on the NNWICE icing platform. We take the NACA0012 airfoil and two-dimensional coronal cylinder as the research objects， and simulate the icing shape under different flow conditions and cloud conditions. The effectiveness of the established calculation method is verified by comparison with the experimental results， and the influence of flow temperature and liquid water content/total water content on icing under mixed phase conditions and ice crystal water cover conditions analyzed. Comparison of the calculation results with and without the erosion effect verifies the significant influence of the ice crystal erosion effect on icing. This work lays a working foundation for further development of numerical simulation calculation of aero engine icing.

Key words: ice crystals/mixed phase icing, adhesion, icing phase transition, erosion, numerical simulation

CLC Number:

V211.41

Yijian MA, Delin CHAI, Xian YI, Jingguo QU, Qiang WANG. Calculation method for ice crystal/mixed phase icing considering ice crystal erosion[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528609-528609.

Figures/Tables 13

Fig.1

Table 1

Formula of shape parameters of hexagonal plate ice crystals

冰晶纵横比（E）	冰晶球形度（ $Φ$ ）	冰晶横向球度（ $Φ ⊥$ ）
$43 π 27 d p a 3$	$4 π 33 + 12 E 93 4 π E 2 / 3$	$2 π 33 93 4 π E 2 / 3$

Table 1

Fig.2

Fig.3

Table 2

Aerodynamic conditions of test-case mix-phase icing conditions of NACA0012 airfoil

算例	来流马赫数 $M a ∞$	来流压力 $p a, ∞$ /Pa	来流温度 $T a, ∞$ /K	来流攻角 $α$ /（°）
10	0.163	98 000	266.18	0
19，20	0.165	98 000	260.65	0

Table 2

Table 3

Cloud conditions of test-case mix-phase icing conditions of NACA0012 airfoil

算例

L W C / (g ⋅ m - 3)

M V D d / μ m

I W C / (g ⋅ m - 3)

M V D i c / μ m

结冰时间

$t a c / s$

0.7

200

600

0.3

0.7

150

600

0.7

0.3

150

600

Table 3

Fig.4

Fig.5

Table 4

Aerodynamic conditions of test-case glaciated icing conditions of curved cylinder

算例	来流马赫数 $M a ∞$	来流压力 $p a, ∞$ /Pa	来流温度 $T a, ∞$ /K	来流攻角 $α$ /（°）	相对湿度RH/%
圆柱算例	0.25	33 000	284.55	0	38

Table 4

Table 5

Cloud conditions of test-case glaciated icing conditions of curved cylinder

算例	$T W C / (g ⋅ m - 3)$	融化率 $η i c / %$	结冰时间 $t a c / s$
17	6	6.0	300
47	4	16.6	320
57	12	14.0	290
67	6	16.6	382
77	6	11.2	300
92	6	26.4	300

Table 5

Fig.6

Fig.7

Fig.8

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Calculation method for ice crystal/mixed phase icing considering ice crystal erosion

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