NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Improved Design Formulae for Buckling of Orthotropic Plates under Combined LoadingSimple, accurate buckling interaction formulae are presented for long orthotropic plates with either simply supported or clamped longitudinal edges and under combined loading that are suitable for design studies. The loads include 1) combined uniaxial compression (or tension) and shear, 2) combined pure inplane bending and 3) shear and combined uniaxial compression (or tension) and pure inplane bending. The interaction formulae are the results of detailed regression analysis of buckling data obtained from a very accurate Rayleigh-Ritz method.
Document ID
20080015745
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Weaver, Paul M. (Bristol Univ. United Kingdom)
Nemeth, Michael P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
April 7, 2008
Subject Category
Structural Mechanics
Meeting Information
Meeting: 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Schaumburg, IL
Country: United States
Start Date: April 7, 2008
End Date: April 10, 2008
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Helicopter Society, Inc., American Society for Composites, American Society of Civil Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available