Optimal Transition of Coaxial Compound Helicopter after Total Propeller Failure-Reference-Cited by-同舟云学术

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Optimal Transition of Coaxial Compound Helicopter after Total Propeller Failure

Published:2024-11 Issue:6 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhao Yanqin¹^ORCID,Yuan Ye²^ORCID,Chen Renliang³

Affiliation:

1. Lecturer, School of General Aviation, Nanchang Hangkong Univ., Nanchang 330063, China. ORCID:

2. Lecturer, Dept. of Aerospace Engineering, Swansea Univ., Swansea, Wales SA2 8PP, UK. ORCID:

3. Professor, National Key Laboratory of Helicopter Aeromechanics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, Jiangsu 210016, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5419

Reference24 articles.

1. Arslan Y. O. 2022. “Optimal trajectory generation and tracking for a helicopter in tail rotor failure.” M.S. thesis Graduate School of Natural and Applied Sciences Middle East Technical Univ.

2. Failure investigations of helicopter tail rotor gearbox casings at Agustawestland Limited

3. Flight Dynamics Modeling, Trim, Stability, and Controllability of Coaxial Compound Helicopters

4. Description of a Dynamical Framework to Analyse the Helicopter Tail Rotor

5. Analysis of low-speed height-velocity diagram of a variable-speed-rotor helicopter in one-engine-failure

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