Experimental Data for Micro Air Vehicles with Pliant Wings in Unsteady Conditions-Reference-Cited by-同舟云学术

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Experimental Data for Micro Air Vehicles with Pliant Wings in Unsteady Conditions

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Babcock Judson¹,Scheffer Roland²,Albertani Roberto³,Abate Gregg¹

Affiliation:

1. U.S. Air Force Research Laboratory

2. German Liaison Office for Defense Materiel USA /Canada

3. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6052

Reference10 articles.

1. Tobak, M. "The Use of the Indicial Function Concept in the Analysis of Unsteady Motions of Wings and Wing-TailCombinations,"NACA Report1188,1954.

2. Etkin,B.,DynamicsofAtmosphericFlight.JohnWileyandSons,Inc.,1972.

3. Blakelock,J.H.,AutomaticControlofAircraftandMissiles.JohnWiley&Sons,Inc.,1965.

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1. Aeroelasticity Validation Study for a Three-Dimensional Membrane Wing;AIAA Journal;2018-06

2. Aeroelasticity Investigation of Generic SUAS-Membrane Wing Validation Study;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

3. Aerodynamic Investigation of Generic SUAS;42nd AIAA Fluid Dynamics Conference and Exhibit;2012-06-25

4. Tip Vorticity and Membrane-Strain Analysis on a MAV Elliptical Pliant Membrane-Wing;6th AIAA Theoretical Fluid Mechanics Conference;2011-06-14

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