Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses
An edition of Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses (1992)
By Govind Rengarajan
Publish Date
1992
Publisher
National Aeronautics and Space Administration,National Technical Information Service, distributor
Language
eng
Pages
-
Description: