Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells
Subtitle: presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category
By: Theodore F. Johnson, Michael F. Card.
Contributors: Card, Michael F.; United States. National Aeronautics and Space Administration.
Series: [NASA technical memorandum] -- 112006.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Thermal buckling.; Cylindrical shells.; Stiffening.; Mechanical properties.; Applications programs (Computers).; Axial loads.; Transatmospheric vehicles.; Digital simulation.; Computerized simulation.
Notes: Shipping list no.: 97-0768-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.