Effects of initial geometric imperfections on the non-linear response of the Space Shuttle superlightweight liquid-oxygen tank

Author:

Nemeth Michael P.,Young Richard D.,Collins Timothy J.,Starnes James H.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference17 articles.

1. Anon., Buckling of thin-walled circular cylinders, NASA Space Vehicle Design Criteria, NASA SP-8007, August 1968.

2. Anon., Buckling of thin-walled truncated cones, NASA Space Vehicle Design Criteria, NASA SP-8019, September 1968.

3. M.P. Nemeth, J.H. Starnes Jr., The NASA monographs on shell stability design recommendations — a review and suggested improvements, NASA TP-1998-206290, January 1998.

4. Nonlinear behavior of Space Shuttle superlightweight liquid-oxygen tank under prelaunch loads;Nemeth;J. Spacecr. Rockets,1999

5. Modeling and non-linear structural analysis of a large-scale launch vehicle;Young;J. Spacecr. Rockets,1999

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