Modeling and Wind Tunnel Test Validation of a Hybrid Compound High-Speed Helicopter-Reference-Cited by-同舟云学术

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Modeling and Wind Tunnel Test Validation of a Hybrid Compound High-Speed Helicopter

Published:2023-12-14 Issue: Volume:36 Page:101-106
ISSN:
Container-title:2023 3rd International Conference on Robotics, Automation and Artificial Intelligence (RAAI)
language:
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Author:

Yin Xinfan¹,Ma Hongxu¹,An Honglei¹,Peng Xianmin²,Zhang Guichuan²,Nie Bowen²

Affiliation:

1. College of Intelligence Science and Technology, National University of Defense Technology,Changsha,China

2. Low Speed Aerodynamics Institute, China Aerodynamics Research and Development Center,Mianyang,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10601248/10601198/10601283.pdf?arnumber=10601283

Reference14 articles.

1. Development overview and key technologies of high speed hybrid helicopter with single main rotor;Huang;Journal of Aerospace Power,2021

2. Development status and key technologies of composite high speed helicopters abroad;Yin;Aerodynamic Missile Journal,2019

3. Progress of compound helicopter technology;Li;Journal of Nanjing University of Aeronautics & Astro-nautics,2016

4. Performance comparison between a conventional helicopter and compound helicopter configurations

5. Current status, development trend and counter-measure for high-speed rotorcraft;Wu;Journal of Nanjing University of Aeronautics & Astronautics,2015

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