Experimental Investigation into the Aerodynamic Properties of a Flexible and Rigid Wing Micro AIr Vehicle-Reference-Cited by-同舟云学术

Experimental Investigation into the Aerodynamic Properties of a Flexible and Rigid Wing Micro AIr Vehicle

Published:2004-06-19 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

DeLuca Anthony¹,Reeder Mark¹,Ol Michael²,Freeman Jacob²,Simonich Michael²,Bautista Ian³

Affiliation:

1. Air Force Institute of Technology

2. Air Force Research Laboratory

3. Air Force Research Lab

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2396

Reference12 articles.

1. McMichael,J.M.,andFrancis,M.S."MicroAirVehicles-TowardaNewDimensioninFlight,"Onlinepaper. December 1997 http://www.darpa.mil/tto/mav/mav_auvsi.html.

2. Kellogg,M.I.andBowman,W.J."ParametricDesignStudyoftheThicknessofAirfoilsatReynoldsNumbers From60,000-150,000." AIAA Paper2004-1054, January2004.

3. Micro-Air-Vehicles: Can They be Controlled Better?

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