Influence of an asymmetric ring on the modeling of an orthogonally stiffened cylindrical shell
By: Naveen Rastogi and Eric R. Johnson.
Contributors: Johnson, Eric R.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA CR-195953.
Publisher: Virginia Polytechnic Institute and State University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Blacksburg, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Asymmetry.; Cylindrical shells.; Fuselages.; Internal pressure.; Reinforced shells.; Reinforcement rings.; Stiffening.; Structural analysis.
Notes: Caption title.

Also available via Internet from the NASA Technical Report Server web site. Address as of 6/21/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19940029756%5F1994029756.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994]. 1 microfiche.