| 舰载飞机纵向逃逸性能仿真研究 |
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| 引用本文： | 崔坤林,胡国才,罗云宝.舰载飞机纵向逃逸性能仿真研究[J].海军航空工程学院学报,2009,24(4):435-439. |
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| 作者姓名： | 崔坤林 胡国才 罗云宝 |
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| 作者单位： | 1. 海军装备部,北京,100076
2. 海军航空工程学院飞行器工程系,山东,烟台,264001 |
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| 摘 要： | 建立了舰载飞机的逃逸动力学分析模型，对飞机在不同着舰条件下的逃逸性能和起落架载荷进行了数值仿真。结果表明，着舰速度越大、发动机推力加速性越好，对飞机的逃逸越有利；舰艇运动会使飞机着舰点偏离理想着舰点并增大起落架载荷；舰尾流对逃逸性能的影响不大，但会使飞机着舰点偏离理想着舰点，不利于飞机的着舰安全。
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| 关 键 词： | 舰载飞机 逃逸性能 起落架载荷 数值仿真 |
Simulated Investigation for Carrier-Based Airplane Longitudinal Go-around Performance |
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| CUI Kun-lin,HU Guo-cai and LUO Yun-bao.Simulated Investigation for Carrier-Based Airplane Longitudinal Go-around Performance[J].Journal of Naval Aeronautical Engineering Institute,2009,24(4):435-439. |
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| Authors: | CUI Kun-lin HU Guo-cai and LUO Yun-bao |
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| Institution: | 1. Naval Equipment Department, Beijing 100076, China; 2. Department of Airborne Vehicle Engineering, NAAU, Yaitai Shandong 264001, China) |
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| Abstract: | A flight dynamic model of carrier-based airplane go-around was presented, tJo-arounu performances and loads of landing-gear were simulated for various carrier landing conditions. Results show that larger approaching speed and engine-power acceleration are benefits for go-around performance. Due to carrier vertical and pitch motions, the landing point on deck may depart from the designated touch point （DTP）, and the landing-gear ioadings rise for some increments. Carrier air wake seems a little affect airplane go-around performance, but makes the landing point apart from the DTP which will affect the airplane landing safety. |
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| Keywords: | carrier-based airplane go-around performance landing-gear load numerical simulation |
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