A Novel Method to Attach Membranes Uniformly on MAV Wings-Reference-Cited by-同舟云学术

A Novel Method to Attach Membranes Uniformly on MAV Wings

Published:2013 Issue: Volume: Page:71-79
ISSN:2191-5644
Container-title:Composite Materials and Joining Technologies for Composites, Volume 7
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Author:

Abudaram Yaakov J.,Rohde Sean,Hubner James Paul,Ifju Peter

Publisher

Springer New York

Link

http://link.springer.com/content/pdf/10.1007/978-1-4614-4553-1_8

Reference13 articles.

1. Mueller TJ (2000) Proceedings of the conference on fixed flapping and rotary wing vehicles at very low Reynolds numbers, Notre Dame University, Indiana, 5–7 June 2000

2. McMichael JM, Col. Francis MS, USAF (1997) Micro air vehicles – toward a new dimension in flight from http://www.fas.org/irp/program/collect/docs/mav_auvsi.htm

3. Ifju PG, Ettinger S, Jenkins D, Martinez L (2001) Composite materials for micro air vehicles (MAV’s). SAMPE J 37(4):7–12

4. Stanford B, Ifju P, Albertani R, Shyy W (2008) Fixed membrane wings for micro air vehicles: experimental characterization, numerical modeling, and tailoring. Prog Aerospace Sci 44:258–294

5. Pisano W, Lawrence D (2008) Autonomous gust insensitive aircraft. In: AIAA guidance, navigation, and control conference, Honolulu, 18–21 Aug 2008

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1. Passive Roll Compensation on Micro Air Vehicles with Perimeter Reinforced Membrane Wings;International Journal of Micro Air Vehicles;2013-09

2. Investigating the Aerodynamic Effects of Flexible Membrane Wings;Conference Proceedings of the Society for Experimental Mechanics Series;2012-09-06