Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy-Reference-Cited by-同舟云学术

Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy

Published:2014-05 Issue:5 Volume:52 Page:964-980
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Cavallaro Rauno¹,Demasi Luciano¹,Passariello Andrea¹

Affiliation:

1. Department of Aerospace Engineering, San Diego State University, San Diego, California 92182

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052242

Reference30 articles.

1. V-Wings and Diamond Ring-Wings of Minimum Induced Drag

2. The joined wing - An overview

3. LangeR. H.CahillJ. F.BradleyE. S.EudailyR. R.JennessC. M.MacwilkinsonD. G. “Feasibility Study of the Transonic Biplane Concept for Transport Aircraft Applications,” NASA CR-132462, 1974.

4. Future of Airplane Aeroelasticity

5. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future

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