Limit Pressure of a Circumferentially Reinforced Sic/Ti Ring

By: Nasa, National Aeronautics and Space Adm

Limit loads under plane stress and plane strain are found for a circumferentially reinforced elastoplastic ring subjected to interior pressure. These are used as bounds on an estimate of the failure pressure of a SiC/Ti test rig that is being fabricated and tested. The ring is to serve as a benchmark against which deformation and failure analysis methods can be assessed. An anisotropic perfect plasticity idealization of the SiC/Ti ring material is made and used in the limit load calculations. An estimate of the failure pressure of the NASA/PW benchmark test ring is given. Robinson, D. N. and Pastor, M. S. Unspecified Center NAG3-379; RTOP 510-01-50...

• Format: Paperback
• Language: English
• ISBN: 1729050360
• ISBN13: 9781729050361
• Release Date: January 1
• Publisher: Independently Published
• Length: 30 Pages
• Weight: 0.21 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"