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Nasa/Army Rotorcraft Technology. Volume 2: Materials and Structures, Propulsion and Drive Systems, Flight Dynamics and Control, and Acoustics.

机译：美国宇航局/陆军旋翼机技术。第2卷：材料和结构，推进和驱动系统，飞行动力学和控制以及声学。

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年度 1988
页码 1-585
总页数 585
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aeroacoustics; Aircraft design; Conferences; Controllability; Engine design; Fracture mechanics; Helicopters; Rotor aerodynamics; Composite structures; Control theory; Crashworthiness; Fatigue (Materials); Gas turbine engines; Human factors engineering; Ice formation;

机译：气动声学;飞机设计;会议;可控性;发动机设计;断裂力学;直升机;转子空气动力学;复合结构;控制理论;耐撞性;疲劳（材料）;燃气涡轮发动机;人因工程;结冰;

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专利

1. Boeing, U.S. Army Test AVMS Rotorcraft Flight Control System [J] . Rotor & Wing . 2012,第4期

机译：美国陆军波音公司测试AVMS旋翼飞机飞行控制系统
2. Dynamic Modeling, Control System Design and MIL-HIL Tests of an Unmanned Rotorcraft Using Novel Low-Cost Flight Control System [J] . Khalesi Mohammad Hossein, Salarieh Hassan, Foumani Mahmoud Saadat Iranian Journal of Science and Technology, Transactions of Mechanical Engineering . 2020,第3期

机译：使用小型低成本飞行控制系统无人旋翼机的动态建模，控制系统设计和密尔-HIL测试
3. Nonlinear robust control of hypersonic aircrafts with interactions between flight dynamics and propulsion systems [J] . Li Zhaoying, Zhou Wenjie, Liu Hao ISA Transactions . 2016,第Null期

机译：高超音速飞机的非线性鲁棒控制与飞行动力学和推进系统之间的相互作用
4. Military Airworthiness for CBM and HUMS: Processes, Policies, Qualification Standards, and Testing for US Army Rotorcraft Propulsion Systems [C] . Tim Rickmeyer, Dan Wade AHS international Airworthiness, CBM and HUMs specialists' meeting . 2013

机译：CBM和HUMS的军事适航性：美国陆军旋翼飞机推进系统的流程，政策，资格标准和测试
5. Integrated flight/propulsion control with variable rotor speed command for rotorcraft. [D] . Iwata, Takanori. 1996

机译：旋翼航空器具有可变旋翼速度指令的集成飞行/推进控制。
6. Modeling the Dynamics of a Non-Limited and a Self-Limited Gene Drive System in Structured Aedes aegypti Populations [O] . Mathieu Legros, Chonggang Xu, Amy Morrison, -1

机译：模拟埃及伊蚊种群中非限制性和自我限制性基因驱动系统的动力学
7. Preliminary design features of the RASCAL: A NASA /Army rotorcraft in-flight simulator [O] . Hindson, William S., Eshow, Michelle M., Doane, Douglas H., 1993

机译：RASCAL的初步设计特征：NASA /陆军旋翼机飞行模拟器

Nasa/Army Rotorcraft Technology. Volume 2: Materials and Structures, Propulsion and Drive Systems, Flight Dynamics and Control, and Acoustics.

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