Simplified design equations for buckling of axially compressed sandwich cylinders with orthotropic facings and core
BERT, C. W. /OKLAHOMA, U., SCHOOL OF AEROSPACE AND MECHANICAL ENGINEERING, NORMAN, OKLA./., REESE, C. D.
Journal of Aircraft ; 6 , 6 ; 515-519
1969-01-01
5 pages
Article (Journal)
Electronic Resource
English