Stability of circular cylindrical shells under transient axial impulsive loading
Contributors: Toronto, Ont. University.
Publisher: s.n.]
Published: 1976
Place of publication: [Toronto
Language: eng
Number of pages: 100
Subjects: Airplanes -- Fuselage; Buckling (Mechanics); Roofs, Shell; Stability of airplanes
Notes: Thesis--University of Toronto.

Vita.

Bibliography: leaves 26-29 (2d group)