Open Access
Issue
JNWPU
Volume 41, Number 3, June 2023
Page(s) 480 - 489
DOI https://doi.org/10.1051/jnwpu/20234130480
Published online 01 August 2023
  1. 李伟李香刘小光et al新概念飞行器的研究现状及发展趋势科技创新与应用 20153467[Article]

    李伟, 李香, 刘小光, 等. 新概念飞行器的研究现状及发展趋势[J]. 科技创新与应用, 2015(34): 67

    [Google Scholar]
  2. LI Wei, LI Xiang, LIU Xiaoguang, et al. Research status and development trend of new concept aircraft[J]. Technology Innovation and Application, 2015(34): 67 [Article] (in Chinese) [Google Scholar]
  3. 宋威艾邦成多体飞行器分离动力学问题研究进展航空学报 2022436025950

    宋威, 艾邦成. 多体飞行器分离动力学问题研究进展[J]. 航空学报, 2022, 43(6): 025950

    [Google Scholar]
  4. SONG Wei, AI Bangcheng. Research progress on separation dynamics of multibody aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(6): 025950 (in Chinese) [Google Scholar]
  5. LIJEWSKI L E, SUHS N E. Time-accurate computational fluid dynamics approach to transonic store separation trajectory prediction[J]. Journal of Aircraft, 1994, 31(4): 886–891 [Article] [CrossRef] [Google Scholar]
  6. 郭正李晓斌瞿章华et al用非结构动网格方法模拟有相对运动的多体绕流空气动力学学报 2001193310316 [Article]

    郭正, 李晓斌, 瞿章华, 等. 用非结构动网格方法模拟有相对运动的多体绕流[J]. 空气动力学学报, 2001, 19(3): 310-316

    [Google Scholar]
  7. GUO Zheng, LI Xiaobin, QU Zhanghua, et al. Simulation of flows past multi-body in relative motion with dynamic unstructured method[J]. Acta Aerodynamica Sinica, 2001, 19(3): 310–316 [Article] (in Chinese) [Google Scholar]
  8. 刘周, 周伟江, 龚安龙. 一种飞行器多体分离模拟方法: 中国, CN102490909A[P]. 2012-06-13

    刘周, 周伟江, 龚安龙. 一种飞行器多体分离模拟方法: 中国, CN102490909A[P]. 2012-06-13

    [Google Scholar]
  9. 铁鸣方洪于盈et al临近空间飞行器多体分离多学科耦合仿真系统系统仿真学报 201830828262833 [Article]

    铁鸣, 方洪, 于盈, 等. 临近空间飞行器多体分离多学科耦合仿真系统[J]. 系统仿真学报, 2018, 30(8): 2826-2833

    [Google Scholar]
  10. TIE Ming, FANG Hong, YU Ying, et al. Multidisciplinary coupling simulation system for multibody separation of adjacent spacevehicles[J]. Journal of Systems Simulation, 2018, 30(8): 2826–2833 [Article] (in Chinese) [Google Scholar]
  11. 董杨彪, 郭叔伟, 王晶晶, 等. 基于混合动网格技术的飞行器多体分离CFD仿真方法及系统: 中国, CN110610065A[P]. 2019-12-24

    董杨彪, 郭叔伟, 王晶晶, 等. 基于混合动网格技术的飞行器多体分离CFD仿真方法及系统: 中国, CN110610065A[P]. 2019-12-24

    [Google Scholar]
  12. 蒋崇文, 胡姝瑶, 高振勋, 等. 飞行器多体分离模拟的重叠网格扰动域更新方法: 中国, CN113962030A[P]. 2022-01-21

    蒋崇文, 胡姝瑶, 高振勋, 等. 飞行器多体分离模拟的重叠网格扰动域更新方法: 中国, CN113962030A[P]. 2022-01-21

    [Google Scholar]
  13. DILLENIUS M F E, GOODWIN F K, NIELSEN J N. Extension of the method for predicting six-degree-of-freedom store separation trajectories at speeds up to the critical speed to include a fuselage with noncircular cross section, I-Theoretical methods, and comparisons with experiment[R]. AFFDL-TR-1974-130 [Google Scholar]
  14. 王竞男刘莉卜奎晨高速动能导弹级间分离动力学分析与仿真弹箭与制导学报 20032355052 [Article]

    王竞男, 刘莉, 卜奎晨. 高速动能导弹级间分离动力学分析与仿真[J]. 弹箭与制导学报, 2003, 23(5): 50-52

    [Google Scholar]
  15. WANG Jingnan, LIU Li, BU Kuichen. Kinetic analysis and simulation of stage separation for hypersonic velocity kinetic energy missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2003, 23(5): 50–52 [Article] (in Chinese) [Google Scholar]
  16. 王鑫袁晓光杨星基于拉格朗日方法的飞行器多体分离姿态动力学分析研究西北工业大学学报 20143211822 [Article]

    王鑫, 袁晓光, 杨星. 基于拉格朗日方法的飞行器多体分离姿态动力学分析研究[J]. 西北工业大学学报, 2014, 32(1): 18-22

    [Google Scholar]
  17. WANG Xin, YUAN Xiaoguang, YANG Xing. Analysis of attitude dynamics of multibody separation of aircraft based on Lagrange method[J]. Journal of Northwestern Polytechnical University, 2014, 32(1): 18–22 [Article] (in Chinese) [Google Scholar]
  18. 蒋增辉, 宋威, 鲁伟, 等. 高速风洞投放模型试验飞行器分离轨迹预测方法及系统: 中国, CN107991053B[P]. 2020-04-10

    蒋增辉, 宋威, 鲁伟, 等. 高速风洞投放模型试验飞行器分离轨迹预测方法及系统: 中国, CN107991053B[P]. 2020-04-10

    [Google Scholar]
  19. 贾洪印, 陈江涛, 张培红, 等. 一种适用于飞行器多体分离相容性度量与表征方法: 中国, CN113609600B[P]. 2021-12-14

    贾洪印, 陈江涛, 张培红, 等. 一种适用于飞行器多体分离相容性度量与表征方法: 中国, CN113609600B[P]. 2021-12-14

    [Google Scholar]
  20. 宋威鲁伟蒋增辉et al内埋武器高速风洞弹射投放模型试验关键技术研究力学学报 201850613461355 [Article]

    宋威, 鲁伟, 蒋增辉, 等. 内埋武器高速风洞弹射投放模型试验关键技术研究[J]. 力学学报, 2018, 50(6): 1346-1355

    [Google Scholar]
  21. SONG Wei, LU Wei, JIANG Zenghui, et al. The crucial technique investigation of wind-tunnel drop-model testing for the supersonic internal weapons[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(6): 1346–1355 [Article] (in Chinese) [Google Scholar]
  22. 艾邦成宋威董垒et al内埋武器机弹分离相容性研究进展综述航空学报 20204110023809[Article]

    艾邦成, 宋威, 董垒, 等. 内埋武器机弹分离相容性研究进展综述[J]. 航空学报, 2020, 41(10): 023809

    [Google Scholar]
  23. AI Bangcheng, SONG Wei, DONG Lei, et al. Review on aircraft-store separation compatibility for the internal weapons[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 023809[Article] (in Chinese) [Google Scholar]

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.