Nonlinear Structural Analysis of an Icosahedron Under an Internal Vacuum-Reference-Cited by-同舟云学术

Nonlinear Structural Analysis of an Icosahedron Under an Internal Vacuum

Published:2015-05 Issue:3 Volume:52 Page:878-883
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Adorno-Rodriguez Ruben¹,Palazotto Anthony N.¹

Affiliation:

1. U.S. Air Force, at Edwards AFB, Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033284

Reference3 articles.

1. Lana-TergiF. “The Aerial Ship,” Aeronautical Soc. of Great Briton, London, 1910.

2. MetlenT. “Design of a Lighter than Air Vehicle that 3Achieves Positive Buoyancy in Air Using a Vacuum,” M.S. Thesis, Air Force Inst. of Technology, Wright–Patterson AFB, OH, June 2013.

3. Adorno-RodriguezR. “Nonlinear Structural Analysis of an Icosahedron and its Application to Lighter than Air Vehicles Under a Vacuum,” M.S. Thesis, Air Force Inst. of Technology, Wright–Patterson AFB, OH, March 2014.

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