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Quantifying Square Membrane Wrinkle Behavior Using MITC Shell ElementsFor future membrane based structures, quantified predictions of membrane wrinkling behavior in terms of amplitude, angle and wavelength are needed to optimize the efficiency and integrity of such structures, as well as their associated control systems. For numerical analyses performed in the past, limitations on the accuracy of membrane distortion simulations have often been related to the assumptions made while using finite elements. Specifically, this work demonstrates that critical assumptions include: effects of gravity. supposed initial or boundary conditions, and the type of element used to model the membrane. In this work, a 0.2 square meter membrane is treated as a structural material with non-negligible bending stiffness. Mixed Interpolation of Tensorial Components (MTTC) shell elements are used to simulate wrinkling behavior due to a constant applied in-plane shear load. Membrane thickness, gravity effects, and initial imperfections with respect to flatness were varied in numerous nonlinear analysis cases. Significant findings include notable variations in wrinkle modes for thickness in the range of 50 microns to 1000 microns, which also depend on the presence of an applied gravity field. However, it is revealed that relationships between overall strain energy density for cases with differing initial conditions are independent of assumed initial con&tions. In addition, analysis results indicate that the relationship between amplitude scale (W/t) and structural scale (L/t) is linear in the presence of a gravity field.
Document ID
20040082044
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Jacobson, Mindy B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Iwasa, Takashi
(Tokyo Univ. Japan)
Natori, M. C.
(Institute of Space and Astronautical Science Sagamihara, Japan)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Structural Mechanics
Meeting Information
Meeting: 45th AIAA Structural Dynamics and Materials Conference
Location: Palm Springs, CA
Country: United States
Start Date: April 19, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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