Design Guidelines of Rotary Wings in Hover for Insect-Scale Micro Air Vehicle Applications-Reference-Cited by-同舟云学术

Design Guidelines of Rotary Wings in Hover for Insect-Scale Micro Air Vehicle Applications

Published:2007-01 Issue:1 Volume:44 Page:252-263
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Tsuzuki Noriaki¹,Sato Shunichi²,Abe Takashi²

Affiliation:

1. University of Tokyo, Tokyo 113-8656, Japan

2. Institute of Space and Astronautical Science/Japanese Aerospace Exploration Agency, Kanagawa 229-8510, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.23165

Reference24 articles.

1. Tsuzuki, N. "A Study on a Miniature Rotary-Wing Vehicle for Mars Exploration: Its Feasibility and Aerodynamic Characteristics of the Rotor," Ph.D. Thesis,Univ. of Tokyo, Tokyo, Japan, 2005.

2. Flight Mechanism of Insect. From Standpoint of View of Bio-Fluiddynamics.

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