Geometrically nonlinear static and dynamic analysis of shells of revolution /

Bibliographic Details
Main Author:	Stricklin, James A. (Author)
Corporate Authors:	Sandia Corporation (sponsoring body.), Manned Spacecraft Center (U.S.) (sponsoring body.), International Union of Theoretical and Applied Mechanics, Symposium on High Speed Computing of Elastic Structures
Other Authors:	Martinez, J. E. (Jose Edwardo), 1943- (Researcher), Haisler, Walter E. (Researcher), Tillerson, J. R. (Researcher), Mebane, P. M. (Researcher), Hong, J. H. (Researcher)
Format:	Conference Proceeding Book
Language:	English
Published:	College Station, Texas : Texas Engineering Experiment Station, [1970]
Subjects:	Shells (Engineering) Structural analysis (Engineering) Nonlinear theories. Loads (Mechanics)

Description
Abstract:	This paper presents the formulation and methods of solution for the geometrically nonlinear analysis of shells of revolution under both symmetric and asymmetric loadings. The static solution is obtained through Newton-Raphson and incremental approaches. Four methods are tried for the dynamic solution with Houbolt's method proving to be the most suitable. Examples are presented for some linear and highly nonlinear problems.
Item Description:	Cover title. "Aerospace Engineering Department, Texas A & M University." "Presented at IUTAM Symposium on High Speed Computing of Elastic Structures, Liege, Belgium, August 25, 1970." Funding information taken from page [i]. "Performing the actual research: J.E. Martinez, W.E. Haisler, J.R. Tillerson, P.M. Mebane, and J.H. Hong"--Page [i].
Physical Description:	25 pages, 18 unnumbered pages : illustrations ; 28 cm
Bibliography:	Includes bibliographical references (pages [27-30]).