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Nonlinear Pressurization and Modal Analysis Procedure for Dynamic Modeling of Inflatable StructuresAn introduction and set of guidelines for finite element dynamic modeling of nonrigidized inflatable structures is provided. A two-step approach is presented, involving 1) nonlinear static pressurization of the structure and updating of the stiffness matrix and 2) hear normal modes analysis using the updated stiffness. Advantages of this approach are that it provides physical realism in modeling of pressure stiffening, and it maintains the analytical convenience of a standard bear eigensolution once the stiffness has been modified. Demonstration of the approach is accomplished through the creation and test verification of an inflated cylinder model using a large commercial finite element code. Good frequency and mode shape comparisons are obtained with test data and previous modeling efforts, verifying the accuracy of the technique. Problems encountered in the application of the approach, as well as their solutions, are discussed in detail.
Document ID
20030014812
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Smalley, Kurt B.
(Clarkson Univ. Potsdam, NY United States)
Tinker, Michael L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Saxon, Jeff
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Publication Information
Publication: Journal of Spacecraft and Rockets
Publisher: Copyright Clearance Center, Inc.
Volume: 39
Issue: 5
ISSN: 0022-4650
Subject Category
Numerical Analysis
Report/Patent Number
ISSN: 0022-4650
Distribution Limits
Public
Copyright
Public Use Permitted.
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