[1] |
宣海军),(陆晓),(洪伟荣),等. 航空发动机机匣包容性研究综述[J]. (航空动力学报), 2010,25(8):1860―1870. Xuan Haijun, Lu Xiao, Hong Weirong, et al. Review of aero-engine case containment research [J]. Journal of Aerospace Power,2010,25(8): 1860―1870. (in Chinese
|
[2] |
Littell J D, Binienda W K, Roberts G D,et al. Characterization of damage in triaxial braided composites under tensile loading [J]. Journal of Aerospace Engineering, 2009,22(3):270―279.
|
[3] |
Ruggeri C. High strain rate data acquisition of 2D braided composite structures [D]. USA: The University of Arkon, 2009.
|
[4] |
Staniszewski M. Simulation of tri-axially braided composites half-cylinder behavior during ballistic impact [D]. USA: The University of Akron, 2007.
|
[5] |
Goldberg R K, Blinzler B J, Binienda W K. Modification of a macromechanical finite-element based model for impact analysis of triaxially braided composites [J]. Journal of Aerospace Engineering, 2012,25(3):383―394.
|
[6] |
Roberts G D, Pereira J M, Jr. Revilock D M, et al. Ballistic impact of braided composite with a soft projectile [J]. Journal of Aerospace Engineering, 2005,18(1):3―7.
|
[7] |
Sutcliffe M P F, Aceves C M, Stronge W J,et al. Moderate speed impact damage to 2D-braided glass-carbon composites [J]. Composite Structures, 2012,94(5):1781―1792.
|
[8] |
FAA/SAE committee on uncontained turbine engine rotor events [R]. Washington, D. C., USA: Federal Aviation Administration,1994.
|
[9] |
Stotler C L, Coppa A P. Containment of composite fan blades [R]. Cleveland Ohio, USA: NASA - Lewis Research Center,1979.
|
[10] |
Stotler C L. Development of advanced lightweight system containment-Final report [R]. Cleveland Ohio, USA: NASA - Lewis Research Center,1981.
|
[11] |
Naik D, Sankaran S, Mobasher B,et al. Development of reliable modeling methodologies for fan blade out containment analysis. Part I: Experimental studies [J]. International Journal of Impact Engineering, 2009,36(1):1―11.
|
[12] |
Stahlecker Z, Mobasher B, Rajan S D,et al. Development of reliable modeling methodologies for engine fan blade out containment analysis. Part II: Finite element analysis [J]. International Journal Impact Engineering, 2009,36(3):447―459.
|
[13] |
Shockey D A, Erlich D C, Simons J W. Improved barriers turbine engine fragments: interim report I [R]. Washington DC, USA: Federal Aviation Administration,2002.
|
[14] |
Roberts G D, Revilock D M, Binienda W K. Impact testing and analysis of composites for aircraft engine fan cases [J]. Journal of Aerospace Engineering, 2002,15(3):104―110.
|
[15] |
刘璐璐),(宣海军),(何庆),等. 复合材料机匣受叶片撞击损伤过程研究[J]. (兵工学报), 2011,32(增刊2):264―268. (in Chinese) Liu Lulu, Xuan Haijun, He Qing, et al. Damage process of composite aero-engine case impact by blade [J]. Acta Armamentari, 2011, 32(Suppl 2): 264―268. (in Chinese
|
[16] |
Matzenmillar A, Lubliner J, Taylor R L. A constitutive model for anisotropic damage in fiber composites [J]. Mechnical Material, 1995,20:125―52.
|
[17] |
Hashin Z. Failure criteria for unidirectional fiber composites [J]. Journal of Applied Mechanics, 1980,47(6):329―334.
|
[18] |
He Qing, Xuan Haijun, Liu Lulu. Perforation of aero-engine fan casing by a single rotating blade [J]. Aerospace Science and Technology, 2013,25(1):234―241.
|