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Current research on shear buckling and thermal loads with PASCO: Panel Analysis and Sizing CodeThe PASCO computer program to obtain the detailed dimensions of optimum stiffened composite structural panels is described. Design requirements in terms of inequality constraints can be placed on buckling loads or vibration frequencies, lamina stresses and strains, and overall panel stiffness for each of many load conditions. General panel cross sections can be treated. An analysis procedure involving a smeared orthotropic solution was investigated. The conservatism in the VIPASA solution and the danger in a smeared orthotropic solution is explored. PASCO's capability to design for thermal loadings is also described. It is emphasized that design studies illustrate the importance of the multiple load condition capability when thermal loads are present.
Document ID
19810024958
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stroud, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Greene, W. H.
(NASA Langley Research Center Hampton, VA, United States)
Anderson, M. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-83206
Report Number: NASA-TM-83206
Meeting Information
Meeting: Intern. Symp. on Optimal Structural Design
Location: Tucson, AZ
Country: United States
Start Date: October 19, 1981
End Date: October 22, 1981
Accession Number
81N33501
Funding Number(s)
PROJECT: RTOP 505-53-53-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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