CLC number: O347.3; V231.91
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2012-02-27
Cited: 7
Clicked: 6876
Qing He, Hai-jun Xuan, Lian-fang Liao, Wei-rong Hong, Rong-ren Wu. Simulation methodology development for rotating blade containment analysis[J]. Journal of Zhejiang University Science A, 2012, 13(4): 239-259.
@article{title="Simulation methodology development for rotating blade containment analysis",
author="Qing He, Hai-jun Xuan, Lian-fang Liao, Wei-rong Hong, Rong-ren Wu",
journal="Journal of Zhejiang University Science A",
volume="13",
number="4",
pages="239-259",
year="2012",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A1100294"
}
%0 Journal Article
%T Simulation methodology development for rotating blade containment analysis
%A Qing He
%A Hai-jun Xuan
%A Lian-fang Liao
%A Wei-rong Hong
%A Rong-ren Wu
%J Journal of Zhejiang University SCIENCE A
%V 13
%N 4
%P 239-259
%@ 1673-565X
%D 2012
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A1100294
TY - JOUR
T1 - Simulation methodology development for rotating blade containment analysis
A1 - Qing He
A1 - Hai-jun Xuan
A1 - Lian-fang Liao
A1 - Wei-rong Hong
A1 - Rong-ren Wu
J0 - Journal of Zhejiang University Science A
VL - 13
IS - 4
SP - 239
EP - 259
%@ 1673-565X
Y1 - 2012
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A1100294
Abstract: An experimental and numerical investigation on the aeroengine blade/case containment analysis is presented. Blade out containment capability analysis is an essential step in the new aeroengine design, but containment tests are time-consuming and incur significant costs; thus, developing a short-period and low-cost numerical method is warranted. Using explicit nonlinear dynamic finite element analysis software, the present study numerically investigated the high-speed impact process for simulated blade containment tests which were carried out on high-speed spin testing facility. A number of simulations were conducted using finite element models with different mesh sizes and different values of both the contact penalty factor and the friction coefficient. Detailed comparisons between the experimental and numerical results reveal that the mesh size and the friction coefficient have a considerable impact on the results produced. It is shown that a finer mesh will predict lower containment capability of the case, which is closer to the test data. A larger value of the friction coefficient also predicts lower containment capability. However, the contact penalty factor has little effect on the simulation results if it is large enough to avoid false penetration.
[1]Ambur, D.R., Jaunky, N., Lawson, R.E., Knight, N.F.Jr, 2001. Numerical simulations for high-energy impact of thin plates. International Journal of Impact Engineering, 25(7):683-702.
[2]Borvik, T., Hopperstad, O.S., Berstad, T., Langseth, M., 2002. Perforation of 12 mm thick steel plates by 20 mm diameter projectiles with flat, hemispherical and conical noses Part II: numerical simulations. International Journal of Impact Engineering, 27(1):37-64.
[3]Carney, K.S., Lawrence, C., Carney, D.V., 2002. Aircraft Engine Blade-Out Dynamics. 7th International LS-DYNA Users Conference, Dearborn, USA. LSTC, California, USA, p.14-17.
[4]Chen, G., Chen, Z.F., Tao, J.L., Niu, W., Zhang, Q.P., Huang, X.C., 2005. Investigation and validation on plastic constitutive parameters of 45 steel. Explosion and Shock Waves, 25(5):451-456 (in Chinese).
[5]Chen, G., Chen, Z.F., Xu, W.F., Chen, Y.M., Huang, X.C., 2007. Investigation on the J-C ductile fracture parameters of 45 steel. Explosion and Shock Waves, 27(2):131-135 (in Chinese).
[6]Cosme, N., Chevrolet, D., Bonini, J., Peseux, B., Cartraud, P., 2002. Prediction of Engine Loads and Damages Due to Fan Blade-Off Event. 43rd AIAA/ASME/ASCE/ AHS/ASC Structures, Structural Dynamics, and Materials Conference, Denver, USA. AIAA, Virginia, USA, Report No. AIAA-2002-1666.
[7]Dey, S., Borvik, T., Hopperstada, O.S., Langseth, M., 2007. On the influence of constitutive relation in projectile impact of steel plates. International Journal of Impact Engineering, 34(3):464-486.
[8]Fan, Z.Q., Gao, D.P., Qin, Z.X., Jiang, T., 2006. Experimental study of 20# steel under tensile impact. Gas Turbine Experiment and Research, 19(4):35-51 (in Chinese).
[9]Goldsmith, W., 1999. Review: Non-ideal projectile impact on targets. International Journal of Impact Engineering, 22(2-3):95-395.
[10]Hallquist, J.O., 2006. LS-DYNA Theoretical Manual. Livermore Software Technology Corporation, California, USA.
[11]He, Q., Xuan, H.J., Liu, L.L., Hong, W.R., Wu, R.R., 2012. Perforation of aero-engine fan casing by a single rotating blade. Aerospace Science and Technology, in press.
[12]Heidari, M., Carlson, D.L., Sinha, S., Sadeghi, R., Heydari, C., Bayoumi, H., Son, J., 2008. An Efficient Multi-Disciplinary Simulation of Engine Fan-Blade out Event Using MD Nastran. 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Schaumburg, USA. AIAA, Virginia, USA, Report No. AIAA-2008-2333.
[13]Jain, R., 2010. Prediction of Transient Loads and Perforation of Engine Casing During Blade-Off Event of Fan Rotor Assembly. Proceedings of the IMPLAST Conference, Providence, USA.
[14]Johnson, G.R., Cook, W.H., 1983. A Constitutive Model and Data for Metals Subjected to Large Strains, High Strain Rates and High Temperatures. Proceedings of the Seventh International Symposium on Ballistics, Hague, the Netherlands, p.541-547.
[15]Johnson, G.R., Cook, W.H., 1985. Fracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressures. Engineering Fracture Mechanics, 21(1):31-48.
[16]Knight, N.F.Jr, Jaunky, N., Lawson, R.E., Ambur, D.R., 2000. Penetration simulation for uncontained engine debris impact on fuselage-like panels using LS-DYNA. Finite Elements in Analysis and Design, 36(2):99-133.
[17]Li, J.J., Xuan, H.J., Liao, L.F., Hong, W.R., Wu, R.R., 2009. Penetration of disk fragments following impact on thin plate. Journal of Zhejiang University-SCIENCE A, 10(5):677-684.
[18]Morris, A.J., Vignjevic, R., 1997. Consistent finite element structural analysis and error control. Computer Methods in Applied Mechanics and Engineering, 140(1-2):87-108.
[19]Ravid, M., Bodner, S.R., 1983. Dynamic perforation of viscoplastic plates by rigid projectiles. International Journal of Engineering Science, 21(6):577-591.
[20]Sarkar, S., Atluri, S.N., 1996. Effects of multiple blade interaction on the containment of blade fragments during a rotor failure. Finite Elements in Analysis and Design, 23(2-4):211-223.
[21]Scheffler, D.R., Zukas, J.A., 2000. Practical aspects of numerical simulation of dynamic events: material interfaces. International Journal of Impact Engineering, 24(8):821-842.
[22]Shmotin, Y.N., Gabov, D.V., 2006. Numerical Analysis of Aircraft Engine Fan Blade-Out. 42nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit, California, USA. AIAA, Virginia, USA, Report No. AIAA-2006-620.
[23]Sinha, S.K., Dorbala, S., 2009. Dynamic loads in the fan containment structure of a turbofan engine. Journal of Aerospace Engineering, 22(3):260-269.
[24]Stallone, M.J., Gallardo, V., Storace, A.F., Bach, L.J., Black, G., Gaffney, E.F., 1983. Blade loss transient dynamic analysis of turbomachinery. AIAA Journal, 21(8):1134-1138.
[25]Teng, X., Wierzbicki, T., 2006. Evaluation of six fracture models in high velocity perforation. Engineering Fracture Mechanics, 73(12):1653-1678.
[26]Wierzbicki, T., Bao, Y., Lee, Y., Bai, Y., 2005. Calibration and evaluation of seven fracture models. International Journal of Mechanical Sciences, 47(4-5):719-743.
[27]Xuan, H.J., Wu, R.R., 2006. Aeroengine turbine blade containment tests using high-speed rotor spin testing facility. Aerospace Science and Technology, 10(6):501-508.
[28]Yu, C.L., Chen, Z.P., Wang, J., Yan, S.J, Yang, L.C., 2012. Effect of weld reinforcement on axial plastic buckling of welded steel cylindrical shells. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 13(2):79-90.
[29]Zukas, J.A., 1990. High Velocity Impact Dynamics. John Wiley & Sons, New York, USA.
[30]Zukas, J.A., Scheffler, D.R., 2000. Practical aspects of numerical simulations of dynamic events: effects of meshing. International Journal of Impact Engineering, 24(9):925-945.
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