Buckling of a thin circular cylindrical shell heated along an axial strip
By: D. W. Hill.
Contributors: Stanford University. Dept. of Aeronautical Engineering
Series: Stanford University.  Dept. of Aeronautical Engineering.  Report -- no. 88
Publisher: Stanford University, Dept. of Aeronautical Engineering
Published: 1959
Place of publication: Stanford, Calif
Number of pages: 91
Notes: Bibliographical references: p. 90-91.

Contract number: AF-49(638)-223