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Structural design analysis of the Tail Landing Gear Bay and the vertical/horizontal stabilizers of the RAH-66 comanche helicopter

机译：RAH-66科曼奇直升机的尾起落架舱和垂直/水平稳定器的结构设计分析

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Approved for public release; distribution is unlimited

机译：批准公开发布；发行是无限的

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Shoop Brian P;
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年度 1997
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原文格式 PDF
正文语种 eng
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1. Design and dynamic analysis of landing gear system in vertical takeoff and vertical landing reusable launch vehicle [J] . Zhang Ming, Xu Dafu, Yue Shuai, Proceedings of the Institution of Mechanical Engineers . 2019,第10期

机译：垂直起飞和垂直着陆可重复使用运载火箭起落架系统的设计和动力学分析
2. Design and dynamic analysis of landing gear system in vertical takeoff and vertical landing reusable launch vehicle [J] . Zhang Ming, Xu Dafu, Yue Shuai, Proceedings of the Institution of Mechanical Engineers . 2019,第10期

机译：垂直起飞和垂直着陆可重复使用发动车辆着陆齿轮系统的设计与动态分析
3. Contemporary Approach to the Design-Systematic and Experimental Provision of Autorotation Landing Safety for a Helicopter with Skid Type Landing Gear [J] . S. A. Mikhailov, D. V. Nedelko Russian Aeronautics . 2012,第2期

机译：滑行式起落架直升机自动旋转着陆安全性设计系统和实验研究的当代方法
4. RAH-66 comanche helicopter flight test simulation station (FTSS) [C] . Major Charles J.Packard AHS international forum . 1999

机译：RAH-66科曼奇直升机飞行测试模拟站（FTSS）
5. Modeling and Analysis of an Active Magnetorheological Seat and Landing Gear System to Protect an Occupant in a Helicopter Crash [D] . King, Caitlin Evelyne. 2018

机译：主动磁流变座椅和着陆齿轮系统的建模与分析，保护乘员在直升机坠机中
6. Helicopter Control Energy Reduction Using Moving Horizontal Tail [O] . Tugrul Oktay, Firat Sal 2015

机译：利用水平尾翼降低直升机控制能量
7. Analysis of potential structural design modifications for the tail section of the RAH-66 Comanche Helicopter. [O] . Tobin Vincent M. 1997

机译：RAH-66科曼奇直升机尾部可能的结构设计修改分析。

Structural design analysis of the Tail Landing Gear Bay and the vertical/horizontal stabilizers of the RAH-66 comanche helicopter

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