Structural Design of Cyclocopter Blade System-Reference-Cited by-同舟云学术

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Structural Design of Cyclocopter Blade System

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

Hwang In Seong¹,Hwang Chang Sup¹,Kim Seung Jo¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2020

Reference7 articles.

1. Yun, C.Y. "A New Vertical Take-off and Landing Aircraft with Cycloidal Blades System : Cyclocopter", Ph.D thesis,Seoul National University,2004

2. Construction and testing of a new aircraft cycloidal propeller

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