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Wang X, He X, Wang T, et al. The influence of the microtexture and orientation of columnar grains on the fatigue crack growth of directed energy deposited Ti-6.5Al-2Zr-Mo-V alloys [J]. Additive Manufacturing, 2020, 35: 101174.
Wang X, He X, Wang T, et al. Internal pores in DED Ti-6.5Al-2Zr-Mo-V alloy and their influence on crack initiation and fatigue life in the mid-life regime [J]. Additive Manufacturing, 2019, 28: 373-93.
Tang D, He X, Wu B, et al. Anisotropic fatigue performance of directed energy deposited Ti-6Al-4V: Effects of build orientation [J]. Materials Science and Engineering: A, 2023, 876: 145112.
Han L, He X, Ning Y, et al. Fatigue damage diagnosis and prognosis for 2024 aluminum plates with center holes: A strain monitoring approach [J]. International Journal of Fatigue, 2023, 170: 107535.
Dang L, He X, Tang D, et al. A fatigue life prediction approach for laser-directed energy deposition titanium alloys by using support vector regression based on pore-induced failures [J]. International Journal of Fatigue, 2022, 159: 106748.
Dong Y, He X, Sun X, et al. Fatigue crack growth of a corner crack at the edge of a hole [J]. International Journal of Fatigue, 2020, 139: 105699.
He X, Dong Y, Li Y, et al. Fatigue crack growth in diffusion-bonded Ti-6Al-4V laminate with unbonded zones [J]. International Journal of Fatigue, 2018, 106: 1-10.
He X, Li T, Li Y, et al. Developing an accelerated flight load spectrum based on the nz-N curves of a fleet [J]. International Journal of Fatigue, 2018, 117: 246-56.
Dong Y, He X, Li Y. Marker load-aided bidirectional fatigue crack growth rate measurement via a semi-elliptical surface crack [J]. International Journal of Fatigue, 2018, 111: 208-19.
Dong Y, He X, Li Y. Effect of interface region on fatigue crack growth in diffusion-bonded laminate of Ti-6Al-4V [J]. International Journal of Fatigue, 2018, 117: 63-74.
Dang L, He X, Tang D, et al. A fatigue life posterior analysis approach for laser-directed energy deposition Ti-6Al-4V alloy based on pore-induced failures by kernel ridge [J]. Engineering Fracture Mechanics, 2023, 289: 109433.
He X, Dong Y, Yang B, et al. A wide range stress intensity factor solution for an eccentrically cracked middle tension specimen with clamped ends [J]. Engineering Fracture Mechanics, 2018, 191: 461-75.
He X, Dong Y, Sui F, et al. Fleet economic life prediction: A probabilistic approach including load spectrum variation and structural property variation [J]. Engineering Fracture Mechanics, 2016, 163: 189-205.
He X, Tan M, Xing J T. An investigation on fatigue crack growth rates through a designed nonsymmetric crack growth test [J]. Engineering Fracture Mechanics, 2012, 96: 510-27.
Tang D, He X, Wu B, et al. The effect of porosity defects on the mid-cycle fatigue behavior of directed energy deposited Ti-6Al-4V [J]. Theoretical and Applied Fracture Mechanics, 2022, 119: 103322.
Wang T, He X, Wang J, et al. Detail fatigue rating method based on bimodal Weibull distribution for DED Ti-6.5Al-2Zr-1Mo-1V titanium alloy [J]. Chinese Journal of Aeronautics, 2022, 35(4): 281-91.
Jiao R, He X, Li Y. Individual aircraft life monitoring: An engineering approach for fatigue damage evaluation [J]. Chinese Journal of Aeronautics, 2018, 31(4): 727-39.
He X, Wang T, Wang X, et al. Fatigue behavior of direct laser deposited Ti-6.5Al-2Zr-1Mo-1V titanium alloy and its life distribution model [J]. Chinese Journal of Aeronautics, 2018, 31(11): 2124-35.
Wang T, He X, Wang X, et al. P-S-N Curve Description of Laser Metal Deposition Ti-6.5Al-2Zr-1Mo-1V Titanium Alloy after Duplex Annealing [J]. Materials, 2019, 12(3): 418.
He X, Sui F, Zhai B, et al. Probabilistic and testing analysis for the variability of load spectrum damage in a fleet [J]. Engineering Failure Analysis, 2013, 33: 419-29.
He X, Dong Y, Zhai B, et al. The fleet life reliability analysis under the 90% severe load spectrum [J]. Engineering Failure Analysis, 2011, 18(1): 394-402.
He X, Zhai B, Dong Y, et al. Safe-life analysis accounting for the loading spectra variability [J]. Engineering Failure Analysis, 2010, 17(5): 1213-20.
He X, Sui F, Dong Y, et al. Relative severity investigation in a severe load spectrum [J]. Engineering Failure Analysis, 2010, 17(7-8): 1509-16.
吴斌,唐鼎承,贺小帆,王天帅,张鑫,李玉海. 激光金属沉积TA15钛合金工字梁疲劳性能研究[J]. 稀有金属,2022,46(05):545-553.
王天帅,贺小帆,王金宇,李玉海. 基于双峰对数正态分布模型的DED-TA15钛合金DFR值估计方法[J]. 航空学报,2022,43(03):232-243.
汪鹏飞,贺小帆,张涵,李玉海. 涂层加速老化与自然曝晒试验的相关性分析[J]. 北京航空航天大学学报,2022,48(01):27-35.
左冉东,贺小帆,李玉海. 耐久性分析相对小裂纹扩展速率公式的参数确定方法[J]. 北京航空航天大学学报,2021,47(12):2594-2601.
朱俊贤,贺小帆,李玉海. 阵风载荷谱的损伤分散性研究[J]. 北京航空航天大学学报,2021,47(10):2129-2137.
颜灿林,贺小帆,李玉海. 一种起落架载荷谱相似性判别方法[J]. 北京航空航天大学学报,2019,45(04):752-759.
贺小帆,朱俊贤. 军用飞机结构耐久性严重谱编制与应用研究进展[J]. 航空学报,2022,43(12):63-76.
李唐,贺小帆,隋芳媛,李玉海. 战斗机机群载荷谱损伤分散系数确定方法[J]. 工程力学,2017,34(04):241-247.
孙晓娜,贺小帆,李玉海. 孔边倒角裂纹当量初始缺陷尺寸的确定方法[J]. 北京航空航天大学学报,2018,44(01):187-195.
唐扬刚,贺小帆,刘文珽,李玉海. 飞机连接结构防护涂层老化损伤量化评估方法[J]. 航空学报,2017,38(01):146-158.
贺小帆,隋芳媛,王天帅,李玉海. 机群结构耐久性分析的裂纹萌生方法[J]. 北京航空航天大学学报,2016,42(05):865-870.
贺小帆,刘家曦,王强,刘文珽. 基于载荷损伤分散的严重谱选取方法初探[J]. 工程力学,2015,32(07):32-37.
贺小帆,刘文珽,孙彦鹏,王向明. 带中心孔的钛合金扩散连接层合板裂纹扩展特性[J]. 工程力学,2015,32(04):244-249.
董颖豪,贺小帆,薛栋,刘文珽. 夹持边界下有限大板中心孔单边裂纹应力强度因子求解[J]. 应用力学学报,2015,32(02):187-191+348.
李唐,贺小帆,刘文珽. 基于Fokker F27机群载荷谱损伤分散性计算分析[J]. 北京航空航天大学学报,2015,41(03):551-558.
贺小帆,董颖豪,李玉海,刘文珽. 综合考虑载荷谱和结构特性分散的概率断裂力学方法[J]. 航空学报,2015,36(04):1142-1149.
曹淑森,贺小帆,杨博霄,刘文珽. 夹持边界条件下表面裂纹应力强度因子求解[J]. 北京航空航天大学学报,2014,40(11):1637-1642.
贺小帆,王强,刘文珽. 基于Fokker 27飞机过载-超越数曲线族的严重超越数包线选取[J]. 航空学报,2013,34(04):840-845.
贺小帆,董彦民,刘彦毛,刘文珽. 独立多细节结构耐久性试验寿命的统计标定[J]. 北京航空航天大学学报,2012,38(06):715-719.
董彦民,贺小帆,刘文珽. 基于不同寿命分布的DFR值换算关系[J]. 北京航空航天大学学报,2011,37(12):1524-1528.
贺小帆,刘彦毛,刘文珽,孙彦鹏,王向明. 含孔钛合金扩散连接止焊层合板裂纹扩展特性试验[J]. 航空材料学报,2011,31(05):77-81.
贺小帆,董彦民,闫友为,刘文珽. 独立多细节结构疲劳寿命分布的数值模拟与分析[J]. 工程力学,2010,27(08):217-222.
梁超,贺小帆. 飞-续-飞谱下7B04-T6铝合金裂纹扩展规律试验研究[J]. 航空材料学报,2010,30(03):74-77.
贺小帆,董彦民,刘文珽. 结构和载荷谱分散性分离的疲劳寿命可靠性[J]. 航空学报,2010,31(04):732-737.
贺小帆,梁超,刘文珽. 腐蚀退化加速因子模型与分析[J]. 机械强度,2010,32(02):299-304.
贺小帆,刘文珽,王忠波,杨洪源,王磊. 预腐蚀对30CrMnSiNi2A连接件疲劳寿命影响的试验研究[J]. 机械强度,2009,31(04):664-669.
贺小帆,刘文珽,向锦武. 基于DFR的疲劳加速腐蚀因子模型与分析[J]. 应用力学学报,2008,(03):445-449+542.
贺小帆,杨洪源,刘文珽. 预腐蚀疲劳退化加速因子研究[J]. 航空动力学报,2008,(07):1328-1333.
贺小帆,刘文珽,向锦武. 腐蚀条件下结构耐久性分析的经济寿命修正方法[J]. 机械强度,2008,(03):455-460.
贺小帆,刘文珽,杨洪源. 铝合金加速腐蚀因子模型与分析[J]. 航空材料学报,2008,(03):77-81.
贺小帆,刘文珽,向锦武. 预腐蚀结构耐久性分析的概率断裂力学方法[J]. 工程力学,2008,(05):39-44.
贺小帆,刘文珽,王忠波,杨洪源,王磊. 预腐蚀对疲劳寿命分布特性及参数影响的初步研究[J]. 航空材料学报,2007,(06):21-26.
贺小帆,刘文珽. 腐蚀条件下使用寿命评定的功能失效概率控制方法[J]. 航空学报,2007,(04):858-863.
贺小帆,刘文珽,杨洪源. 基于Weibull分布的疲劳加速腐蚀因子分析[J]. 北京航空航天大学学报,2007,(02):154-158.
贺小帆,刘文珽,向锦武. 基于C—T曲线的加速腐蚀因子分析[J]. 机械强度,2006,(06):888-892.
贺小帆,王磊,刘文珽,向锦武. 基于威布尔分布的C-T曲线通用性分析[J]. 北京航空航天大学学报,2005,(12):1293-1298.
贺小帆,刘文珽,向锦武. 腐蚀条件下结构耐久性分析裂纹扩展规律研究[J]. 强度与环境,2005,(04):53-59.