[1]PAN Y, YU K.Parachute free airdrop packaging box application environmental testing technology overview[J].Highlights in Science, Engineering and Technology, 2023, 72(0):1147-1151[2]姜涛, 鲁航, 田德宇.精确空投系统研究进展及趋势[J]. 现代防御技术, 2024: 1-8.[3]JIANG T, LU H, DEYV T.Research progress and trend on precision airdrop system [J]. Modern Defence Technology: 1-8. (in Chinese)[4]XUE F, REN Y P, LI Z, et al.Aerodynamic characteris-tics of store during lateral jet assisted separation from cavity using free drop technique[J].Chinese Journal of Aeronautics, 2023, 36(1):139-151[5]CHIN D, GRANLUND K, MAATZ I, et al.Stochastic store trajectory of ice models from a cavity into super-sonic flow[J].Journal of Aircraft, 2019, 56(4):1313-1319[6]LOUPY G J M, BARAKOS G N, TAYLOR N J.Store release trajectory variability from weapon bays using scale-adaptive simulations[J].AIAA Journal, 2018, 56(2):752-764[7]宋威, 艾邦成.多体分离动力学研究进展[J].航空学报, 2022, 43(09):025950-[8]SONG W, AI B C.Multibody separation dynamics: Re-view[J].Acta Aeronautica et Astronautica Sinica, 2022, 43(9):025950-[9]宋威, 艾邦成.多体空气动力学研究进展[J].力学学报, 2022, 54(06):1461-1484[10]SONG W, AI B C.Research progress on multibody aer-odynamics[J].Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(6):1461-1484[11]吴卓恒, 余莉, 赵晓舜, 等.前体尾流对降落伞工作性能的影响[J].北京航空航天大学学报, 2021, 47(12):2552-2559[12]WU Z H, YU L, ZHAO X S, et al.Effects of capsule wake on parachute working performance[J].Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(12):2552-2559[13]ZHANG X.Compressible cavity flow oscillation due to shear layer instabilities and pressure feedback[J].AIAA Journal, 1995, 33(8):1404-1411[14]SONG W, AI B C.Analysis of aircraft-store compatibil-ity for internal weapons separation [J]. Aerospace Sci-ence and Technology, 2021, 110: 1-10.[15]SONG W, AI B C, ZHAO X J, et al.Influence of con-trol device on store separation from an open cavity [J]. Aerospace Science and Technology, 2020, 106: 1-11.[16]张兵, 侯明, 王殿宇, 等.迎角对导弹初始弹射弹道的影响[J].兵工学报, 2021, 42(02):438-448[17]ZHANG B, HOU M, WANG D Y, et al.Influence of angle of attack on initial ejection trajectory of missile[J].ACTA Armamentarii, 2021, 42(02):438-448[18]周伟.基于嵌套网格的内埋物单侧投放影响研究[J].飞行力学, 2023, 41(05):30-36[19]ZHOU W.Research on the influence of unilateral store separation from internal bay based on embedded grid[J].Flight Dynamics, 2023, 41(05):30-36[20]YANG X, YU L, LIU M, et al.Fluid structure interac-tion simulation of supersonic parachute inflation by an interface tracking method[J].Chinese Journal of Aero-nautics, 2020, 33(6):1692-1702[21]侯夏伊, 胡俊, 于勇.十字形伞有限质量充气展开及尾流再附现象 [J]. 兵工学报, 2024: 1-11.[22]HOU X Y, HU J, YV Y.Finite mass inflation and wake recontact phenomenon of cross parachutes[J]. ACTA Armamentarii, 2024: 1-11. (in Chinese)[23]TIAN S L, FU J W, CHEN J T.A numerical method for multi-body separation with collisions [J]. Aerospace Science and Technology, 2021, 109: 106426.[24]PETERS N, WISSINK A, EKATERINARIS J.A Mode Based Reduced Order Model for Rotorcraft Store Sepa-ration [C]//AIAA SCITECH 2022 Forum. 2022: 1-17.[25]PETERS N, EKATERINARIS J, WISSINK A.A mode based reduced order model for supersonic store separa-tion [C]//AIAA Aviation 2021 Forum. 2021: 1-19.[26]PETERS N, EKATERINARIS J, WISSINK A.Mode based reduced order model for a moving store [C]//AIAA Scitech 2021 Forum. 2021: 1-38.[27]LI Y J, QU C Y, LI J, et al.Modelling of parachute airborne clusters flight dynamics and parachute interac-tions[J].Aerospace, 2023, 10(51):1-14[28]ZHANG S Y, YU L, MASARATI P, et al.New general correlations for opening shock factor of ram-air para-chute airdrop system [J]. Aerospace Science and Tech-nology, 2022, 129: 107844.[29]贾贺, 邹天琪, 荣伟, 等.不同行星大气下直径比对降落伞气动特性的影响研究[J].航天返回与遥感, 2023, 44(1):70-83[30]JIA H, ZOU T Q, RONG W, et al.Influence of diameter ratio on the aerodynamic performance of parachute sys-tem under different atmospheric conditions[J].Space-craft Recovery & Remote Sensing, 2023, 44(1):70-83[31]黄明星, 王文强, 李健, 等.基于有效透气量对火星降落伞气动力系数预测分析[J].宇航学报, 2020, 41(9):1132-1140[32]HUANG M X, WANG W Q, LI J, et al.Prediction and analysis of aerodynamic coefficient of parachute under Mars conditions based on effective porosity[J].Journal of Astronautics, 2020, 41(9):1132-1140[33]尤因.回收系统设计指南 [M]. 北京: 航空工业出版社, 1988.[34]Ewing E G, Bixby H W, Knacke T W.Recovery Sys-tems Design Guide [M]. Beijing: Aviation Industry Press, 1988.[35]王利荣.降落伞理论与应用 [M]. 北京:宇航出版社, 1997.[36]WANG L R.Theory and Application of Parachutes [M]. Beijing: Astronautics Press, 1997.[37]刘康, 包文龙, 薛晓鹏, 等.环帆伞解除收口充气展开过程数值模拟及应用[J].航天返回与遥感, 2023, 44(03):21-31[38]LIU K, BAO W L, XUE X P, et al.Inflatable simulation research and application of reefed ringsail parachute[J].Spacecraft Recovery & Remote Sensing, 2023, 44(3):21-31[39]BERGERON K, GHOREYSHI M, NOETSCHER G, et al.Computational study of single and clustered para-chutes in the wake of an aircraft [J]. Aerospace Science and Technology, 2022, 127: 1-14.[40]HEIM E R.CFD Wing/Pylon/Finned Store Mutual In-terference Wind Tunnel Experiment [M]. 1991.[41]殷克功, 刘荣忠, 徐刚, 等.末敏弹减速伞充气过程有限元方法研究 [J]. 系统仿真学报, 2009, (9): 2500-2502.[42]YIN K G, LIU R Z, XV G, et al.Research on drag par-achute inflation process of target-sensitivity projectile based on finite element method [J]. Journal of System Simulation, 2009, (9): 2500-2502.[43]廖前芳.物伞系统回收过程动力学仿真与分析 [D]; 国防科学技术大学, 2005.[44]MIU Q F.The Dynamic Simulation and Analysis for a Parachute Payload System During the Recovery Process [D]; National University of Defense Technology, 2005.[45]陈晨, 郭琪磊.一种基于任意拉格朗日-欧拉方法的降落伞充气展开数值模型[J].科学技术与工程, 2021, 21(02):801-807[46]Chen C, Guo Q L.A numerical model of parachute de-ployment inflation process based on arbitrary Lagrange-Euler method[J].Science Technology and Engineering, 2021, 21(2):801-807 |