The exact solution for linear thermoelastic axisymmetric deformations of generally laminated circular cylindrical shells
By: Michael P. Nemeth and Marc R. Schultz
Contributors: United States. National Aeronautics and Space Administration; Langley Research Center; Schultz, Marc R., author
Series: [NASA technical paper] -- NASA/TP 2012-217342; NASA technical paper -- 217342
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 2012
Place of publication: Hampton, Va
Language: eng
Number of pages: 99
Subjects: Anisotropy; Cylindrical shells; Boundary conditions; Composite structures; Surface temperature; Temperature distribution; Thermoelasticity; Laminates; Axial strain
Notes: Title from title screen (viewed Jan. 31, 2013).

"February 2012."

Includes bibliographical references (pages 50-52).

L-20112

869021.04.07.01.13