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Improved Model of Landing-Gear Drop Dynamics

2014; American Institute of Aeronautics and Astronautics; Volume: 51; Issue: 2 Linguagem: Inglês

10.2514/1.c032551

1533-3868

Xiaohui Wei, Chenglong Liu, Liu Xiang-yao, Hong Nie, Yizhou Shao,

Hydraulic and Pneumatic Systems

No AccessEngineering NoteImproved Model of Landing-Gear Drop DynamicsXiaohui Wei, Chenglong Liu, Xiangyao Liu, Hong Nie and Yizhou ShaoXiaohui WeiCollege of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China, Chenglong LiuCollege of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China, Xiangyao LiuCollege of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China, Hong NieCollege of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of China and Yizhou ShaoCollege of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People's Republic of ChinaPublished Online:3 Apr 2014https://doi.org/10.2514/1.C032551SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Milwitzky B. and Cook F. E., "Analysis of Landing-Gear Behavior," NACA, Rept. 1154, 1953. Google Scholar[2] Nie H., "Dynamic Behavior Analysis and Design as Well as Life Prediction Method of Landing Gear," Ph.D. Dissertation, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu, PRC, 1990. Google Scholar[3] Wahi M. K., "Oleo-Pneumatic Shock Strut Dynamic Analysis and Its Real-Time Simulation," Journal of Aircraft, Vol. 13, No. 4, 1976, pp. 303–308. doi:https://doi.org/10.2514/3.44526 JAIRAM 0021-8669 LinkGoogle Scholar[4] Wahi M. K., "Oil Compressibility and Polytropic Air Compression Analysis for Oleo-Pneumatic Shock Struts," Journal of Aircraft, Vol. 13, No. 7, 1976, pp. 527–530. doi:https://doi.org/10.2514/3.44540 JAIRAM 0021-8669 LinkGoogle Scholar[5] Sui F. C. and Lu H., "Mathematical Model Research on Aircraft Landing Gear Damper," Aircraft design, Vol. 2, 2001, pp. 44–51. Google Scholar[6] Chester D. H., "Aircraft Landing Impact Parametric Study with Emphasis on Nose Gear Landing Conditions," Journal of Aircraft, Vol. 39, No. 3, 2002, pp. 394–403. doi:https://doi.org/10.2514/2.2964 JAIRAM 0021-8669 LinkGoogle Scholar[7] Evans P., Perhinschi M. and Mullins S., "Modeling and Simulation of a Tricycle Landing Gear at Normal and Abnormal Conditions," AIAA Modeling and Simulation Technologies Conference, AIAA Paper 2010-7618, Aug. 2010. LinkGoogle Scholar[8] Batterbee D. C., Sims N. D., Stanway R. S. and Wolejzsa Z., "Design and Performance Optimization of Magneto-Rheological Oleo Pneumatic Landing Gear," Proceedings of SPIE, Vol. 5760, No. 1, 2005, pp. 77–88. Google Scholar[9] Gerardi A. G., "Digital Simulation of Flexible Aircraft Response to Symmetrical and Asymmetrical Runway Roughness," U.S. Air Force Flight Dynamics Lab., TR-77-37, Wright-Patterson Air Force Base, Ohio, 1977. CrossrefGoogle Scholar[10] Cook F. E. and Milwitzky B., "Effect of Interaction on Landing-Gear Behavior and Dynamic Loads in a Flexible Airplane Structure," NACA TN-3467, 1955. Google Scholar[11] Wei X. H. and Nie H., "Dynamic Analysis of Aircraft Landing Impact Using Landing-Region-Based Model," Journal of Aircraft, Vol. 42, No. 6, 2005, pp. 1631–1637. doi:https://doi.org/10.2514/1.6801 JAIRAM 0021-8669 LinkGoogle Scholar[12] Wei X. H., Ben L. L., Nie H. and Zhang M., "Analysis of the Anti-Vibration Holdback Device of Carrier-Based Aircraft," Journal of Nanjing University of Aeronautics & Astronautics, Vol. 45, No. 1, 2013, pp. 1–7. Google Scholar[13] Khapane P. D., "Simulation of Asymmetric Landing and Typical Ground Maneuvers for Large Transport Aircraft," Aerospace Science and Technology, Vol. 7, No. 8, 2003, pp. 611–619. doi:https://doi.org/10.1016/S1270-9638(03)00066-X ARSTFZ 1270-9638 CrossrefGoogle Scholar[14] Daniels J. N., "A Method for Landing Gear Modeling and Simulation with Experimental Validation," NASA CR-201601, 1976. Google Scholar[15] Clark A. B., "An Investigation of Classical Dynamic Scaling Techniques Applied to an Oleo-Pneumatic Landing Gear Strut," Air Force Wright Aeronautical Laboratories TR-86-3058, 1987. Google Scholar[16] Liu L. L., Liu H. Z., Wu X. Y. and Wang Z. M., "An Overview of Friction Models in Mechanical Systems," Advances in Mechanics, Vol. 38, No. 2, 2008, pp. 201–211. Google Scholar Previous article Next article