Acoustic measurements of a full-scale coaxial helicopter-Reference-Cited by-同舟云学术

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Acoustic measurements of a full-scale coaxial helicopter

Published:1983-04-11 Issue: Volume: Page:
ISSN:
Container-title:8th Aeroacoustics Conference
language:
Short-container-title:

Author:

MOSHER M.¹,PETERSON R.¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1983-722

Reference9 articles.

1. Rotor radius, R Number of rotors Blades per rotor Rotor separation Blade tip chord Blade taper ratio Blade twist (nonlinear) Solidity, a Referencesrea, S Blade precone angle Blade prelag angle Shaft tilt 5.5 m 2 3 0.76 m 0.29 m 2:1 -10 deg 0.13 12.0 m2 3 deg 1.4 deg

Cited by 3 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. Learning-based modeling and control design for a coaxial helicopter with aerodynamic coupling;Transactions of the Institute of Measurement and Control;2024-03-15

2. Aerodynamic characteristics of rigid coaxial rotor by wind tunnel test and numerical calculation;Chinese Journal of Aeronautics;2019-03

3. A review of helicopter rotor blade tip shapes;Progress in Aerospace Sciences;2013-01

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