[1] |
QIU L J, SONG W B. Efficient decoupled hydrodynamic and aerodynamic analysis of amphibious aircraft water takeoff process[J]. Journal of Aircraft, 2013, 50(5):1369-1379.
|
[2] |
CAMPBELL J C, VIBNJEVIC R. Simulating structural response to water impact[J]. International Journal of Impact Engineering, 2012,49:1-10.
|
[3] |
中国民用航空总局.中国民用航空规章第25部运输类飞机适航标准[S]. 北京:中国民用航空局, 2011. Civil Aviation Administration of China. China civil aviation regulations part 25 airworthiness standard of transport aircraft[S]. Beijing:Civil Aviation Administration of China, 2011(in Chinese).
|
[4] |
中国人民解放军总装备部.军用飞机结构强度规范:地面试验[S]. 北京:中国人民解放军总装备部, 2008 Chinese PLA General Armament Department. Military airplane structural strength specification:Ground tests[S]. Beijing:Chinese PLA General Armament Department, 2008(in Chinese).
|
[5] |
覃湘桂,徐维民,刘海峰,等. 大变形条件下机翼法向载荷的随动加载技术[J]. 南京航空航天大学学报,2018, 50(5):640-664. QIN X G, XU W M, LIU H F, et al. Tracking loading technology of wing's normal force under large deformation condition[J]. Journal of Nanjing University of Aeronautics & Astronautics,2018, 50(5):640-664(in Chinese).
|
[6] |
张彦敏,周贤宾. 飞机蒙皮拉伸成形加载轨迹设计及优化[J]. 北京航空航天大学学报,2017,33(7):826-829. ZHANG Y M, ZHOU X B. Optimization of loading trajectory for skin stretch forming process[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017,33(7):826-829(in Chinese).
|
[7] |
何德华,李东升,李小强. 飞机蒙皮包覆拉伸成形加载轨迹设计优化方法[J]. 塑性工程学报,2009, 16(6):102-106. HE D H, LI D S, LI X Q. Design and optimization of the loading trajectory in aircraft skin drape forming process[J]. Journal of Plastic Engineering,2009,16(6):102-106(in Chinese).
|
[8] |
WANG L, XIE C, YANG C. Static aeroelastic analysis of flexible aircraft with large deformations[C]//AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference.Reston:AIAA,2013.
|
[9] |
何志全,刘杨,李泽江. 大型民用飞机缝翼全尺寸静力试验载荷设计[J].航空学报,2019,40(2):522197. HE Z Q, LIU Y, LI Z J. Load design for full scale static test of slat on large civil aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019,40(2):522197(in Chinese).
|
[10] |
PETR V, ALES P. Using wing model deformation for improvement of CFD results of ESWIRP project[J]. Ceas Aeronautical Journal, 2018, 9(2):361-372.
|
[11] |
EVELYN W, CHRISTOPH W, THOMAS H. Effect of wing deformation on highlift systems of transport aircraft[J]. Pamm, 2009, 9(1):129-130.
|
[12] |
ABBASOV I B, OREKHOV V V. Computational modeling of multipurpose amphibious aircraft Be-200[J]. Advances in Engineering Software, 2014, 69(3):12-17.
|
[13] |
YANG X, WANG T, LIANG J, et al. Survey on the novel hybrid aquatic-aerial ampphibious aircraft:Aquatic unmanned aerial vehicle (AquaUAV)[J]. Progress in Aerospace Sciences, 2015, 74:131-151.
|
[14] |
郑建军,唐吉运,王彬文.C919飞机全机静力试验技术[J].航空学报,2019,40(1):522364. ZHENG J J, TANG J Y, WANG B W. Static test technology for C919 full-scale aircraft structure[J]. Acta Aeronautica et Astronautica Sinica,2019,40(1):522364(in Chinese).
|
[15] |
刘玮, 滕青, 刘冰. 基于地板结构的机身双层双向加载技术[J]. 航空学报, 2018, 39(5):221712. LIU W, TENG Q, LIU B. Double-deck bi-directional loading technology based on airliner cabin floor structure[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(5):221712(in Chinese).
|
[16] |
庞宝才,董登科,弓云昭,等.襟缝翼可动翼面的随动加载方法研究[J].机械科学与技术, 2014,33(10):1590-1593. PANG B C, DONG D K, GONG Y Z, et al. Study on tracking loading method of locomotory wing for flap and slat[J]. Mechanical Science and Technology for Aerospace Engineering,2014,33(10):1590-1593(in Chinese).
|
[17] |
王睿,周洲,祝小平,等.几何非线性机翼本征梁元素模型的高效化改进[J].航空学报,2013,34(6):1309-1318. WANG R, ZHOU Z, ZHU X P, et al. Improving the geometrically nonlinear intrinsic beam element model of wing for high Efficiency[J]. Acta Aeronautica et Astronautica Sinica, 2013,34(6):1309-1318(in Chinese).
|
[18] |
HOZHABROSSADATI S M, CHALLAMEL N, REZAIEE-PAJAND M, et al. Application of Green's function method to bending of stress gradient nanobeams[J]. International Journal of Solids & Structures, 2018, 143:S0020768318301173
|
[19] |
李银山. Maple材料力学[M]. 北京:机械工业出版社, 2009. LI Y S. Maple material mechanics[M]. Beijing:Mechanical Industry Press, 2009(in Chinese).
|
[20] |
薛帮猛,张文升,孙学卫,等. 动力干扰下宽体客机机翼多目标优化设计[J]. 航空学报,2019,40(2):522381. XUE B M, ZHANG W S, SUN X W, et al. Multi-objective wing shape optimization for a wide-body civil aircraft in wingbody-pylon-powered nacelle configuration[J]. Acta Aeronautica et Astronautica Sinica, 2019,40(2):522381(in Chinese).
|
[21] |
SAATY T L, VARGAS L G. Models, methods, concepts & applications of the analytic hierarchy process[J]. International, 2017, 7(2):159-172.
|
[22] |
吴春明, 陈治, 姜明. 蚁群算法中系统初始化及系统参数的研究[J]. 电子学报, 2006, 34(8):1530-1533. WU C M, CHEN Z, JIANG M. The research on Initialization of ants system and configuration of parameters for different TSP problems in ant algorithm[J]. Acta Electronica Sinica, 2006, 34(8):1530-1533(in Chinese).
|
[23] |
罗明强,冯昊成,刘虎,等.机翼结构有限元的快速建模及自动化调整[J]. 北京航空航天大学学报, 2011, 37(6):680-684. LUO M Q, FENG H C, LIU H, et al. Rapid wing structural finite element modeling and automated adjustment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(6):680-684(in Chinese).
|
[24] |
TANG J, XI P, ZHANG B, et al. A finite element parametric modeling technique of aircraft wing structures[J]. Chinese Journal of Aeronautics, 2013,26(5):1202-1210.
|
[25] |
WEN Q, GUO S, HAO L I, et al. Nonlinear dynamics of a flapping rotary wing:Modeling and optimal wing kinematic analysis[J]. Chinese Journal of Aeronautics, 2018, 31(5):1041-1052.
|