RESEARCH PAPERS
Muir, E. R., and Freidmann, P. P., “Forced and aeroelastic responses of bird-damaged fan blades: A comparison and its implications,” Journal of Aircraft, Vol. 53, No. 2, 2016, pp. 561-577.
10.2514/1.C033424Sun, Y., Zhang, Y., Zhou, Y., Zhang, H., Zeng, H., and Yang, K., “Evaluating impact damage of flat composite plate for surrogate bird-strike testing of aeroengine fan blade,” Journal of Composites Science, Vol. 5, No. 7, 2021, pp. 171.
10.3390/jcs5070171Duo, P., Golowin, A., Schaefer, R., Bernhardt, U., Fueller, M., and Pianka, C., “Simulated Foreign Object Damage on Blade Aerofoils: Real Damage Investigation,” In Turbo Expo: Power for Land, Sea, and Air, Berlin, Germany, Vol. 43154, pp. 169-176, Jun 2008.
10.1115/GT2008-50371Sayma, A. I., Kim, M., and Smith, N. H. S., “Leading-Edge Shape and Aeroengine Fan Blade Performance,” Journal of Propulsion and Power, Vol. 19, No. 3, 2003, pp. 517-520.
10.2514/2.6137Liu, H., Che, M. M. H., and Low, K. H., “UAV Airborne Collision to Manned Aircraft Engine: Damage of Fan Blades and Resultant Thrust Loss,” Aerospace Science and Technology, Vol. 113, 2021, p. 106645.
10.1016/j.ast.2021.106645Zhang, J., Chen, Y., Jin, L., Tang, X., and Wang, Z., “Evaluation of the Free-Windmilling Rotational Speed of a Damaged Wide-Chord Fan Rotor,” Aerospace Science and Technology, Vol. 140, 2023, p. 108421.
10.1016/j.ast.2023.108421Lee, S., Jeong, S., Choi, B., Kim, H., and Kim, K., “A Numerical Study for the Effect of Rotor Blade Damaged by FOD on Flow Characteristics of Transonic Axial Compressor,” Journal of the Korean Society of Propulsion Engineers, Vol. 27, No. 6, 2023, pp. 21-31.
10.6108/KSPE.2023.27.6.021Park, G., Kim, K., Kim, S., Kim, Y., and Jeong, S., “Analysis of the Effect of Leading Edge Damage Caused by FOD on the Aerodynamic Performance of Aircraft Fan Blades,” Journal of the Korean Society of Propulsion Engineers, Vol. 29, No. 5, 2025, pp. 1-11.
10.6108/KSPE.2025.29.5.001Rossmann, A., and Institute of Thermal Turbomachinery and Machine Dynamics, “Aeroengine Safety,” World Wide Web, https://aeroenginesafety.tugraz.at/doku.php?id=5:52:521:521, Version 127.0.0.1 (accessed Sep. 10, 2025)
Li, Y., and Sayma, A., “Effects of blade damage on the performance of a transonic axial compressor rotor,” Turbo Expo: Power for Land, Sea, and Air, Copenhagen, Denmark, Vol. 44748, pp. 2427-2437, Jun 2012.
10.1115/GT2012-68324Strazisar, A. J., Wood, J. R., Hathaway, M. D., and Suder, K. L., “Laser Anemometer Measurements in a Transonic Axial-Flow Fan Rotor,” NASA TM-102279, 1989.
Hathaway, M. D., “Unsteady Flows in a Single-Stage Transonic Axial-Flow Fan Stator Row,” NASA TM-88929, 1986.
F.A.A., “Foreign Object Debris Characterization at a Large International Airport,” DOT/FAA/TC-TN14/48, 2015.
Ilieva, G. I., “A Deep Insight to Secondary Flows,” Defect and Diffusion Forum, Vol. 379, 2017, pp. 83-107.
10.4028/www.scientific.net/DDF.379.83Miller, G. R., Lewis, G. W., and Hartmann, M. J., “Shock Losses in Transonic Compressor Blade Rows,” Journal of Engineering for Power, Vol. 83, No. 3, 1961, pp. 235-241.
10.1115/1.3673182Koch, C. C., and Smith, L. H., Jr., “Loss Sources and Magnitudes in Axial-Flow Compressors,” Journal of Engineering for Power, Vol. 98, No. 3, 1976, pp. 411-424.
10.1115/1.3446202Grant, R. J., Johnson, C. G., and Wilkinson, D. H., “Effect of Casing Separations and Tip Leakage Jets on Turbine Efficiency,” International Journal of Heat and Fluid Flow, Vol. 4, No. 4, 1983, pp. 239-245.
10.1016/0142-727X(83)90054-1- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of the Korean Society of Propulsion Engineers
- Journal Title(Ko) :한국추진공학회지
- Volume : 30
- No :1
- Pages :61-71
- Received Date : 2025-10-22
- Revised Date : 2025-11-27
- Accepted Date : 2025-12-30
- DOI :https://doi.org/10.6108/KSPE.2026.30.1.061


Journal of the Korean Society of Propulsion Engineers








