Effects of Asymmetric Blade-Pitching Kinematics on Forward-Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor-Reference-Cited by-同舟云学术

Effects of Asymmetric Blade-Pitching Kinematics on Forward-Flight Performance of a Micro-Air-Vehicle-Scale Cycloidal-Rotor

Published:2016-09 Issue:5 Volume:53 Page:1568-1573
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Benedict Moble¹,Jarugumilli Tejaswi²,Chopra Inderjit²

Affiliation:

1. Texas A&M University, College Station, Texas 77843

2. University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033558

Reference6 articles.

1. Review of Historic and Modern Cyclogyro Design

2. Challenges Facing Future Micro-Air-Vehicle Development

3. Development of a Four-Rotor Cyclocopter

4. BenedictM. “Fundamental Understanding of the Cycloidal-Rotor Concept for Micro Air Vehicle Applications,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Maryland, College Park, MD, Dec. 2010.

5. Experimental Optimization of MAV-Scale Cycloidal Rotor Performance

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