Trim investigation for coaxial rigid rotor helicopters using an improved aerodynamic interference model-Reference-Cited by-同舟云学术

Trim investigation for coaxial rigid rotor helicopters using an improved aerodynamic interference model

Published:2019-02 Issue: Volume:85 Page:293-304
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Yuan Ye^ORCID,Chen Renliang,Li Pan

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Flight dynamics investigation of compound helicopter configurations;Ferguson;J. Aircr.,2014

2. Optimum design of a compound helicopter;Yeo;J. Aircr.,2009

3. D.A. Darrow, F.P. Bertolotti, T.L. Sbabo, F.P. D'anna, inventors; Sikorsky Aircraft Corp, assignee. De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing. United States patent US 7,621,480. 2009 Nov. 24.

4. Interactional aerodynamics and acoustics of a propeller-augmented compound coaxial helicopter;Kim,2008

5. Aeromechanics analysis of a coaxial rotor system in hover and high-advance-ratio forward flight;Feil,2016

Cited by 26 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear dynamic inversion based full envelope robust flight control for coaxial compound helicopter;Aerospace Science and Technology;2024-11

2. Development of a Mathematical Model of a Coaxial Compound Helicopter for Trimming and Stability Analysis;Journal of Aerospace Engineering;2024-09

3. Real-time optimization control of variable rotor speed based on Helicopter/ turboshaft engine on-board composite system;Energy;2024-08

4. An rVPM-Based Aerodynamic Hybrid Optimization Method for Coaxial Rotor with Differentiated Upper and Lower Blades in Both Hover and High-Speed Cruising States;Aerospace;2024-06-09

5. A high-resolution numerical investigation of unsteady wake vortices for coaxial rotors in hover;Chinese Journal of Aeronautics;2024-06