Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration
Accuracy of modal stress calculations by the finite element method
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 7TH ; 1969 ; NEW YORK, NY
1970-03-01
Miscellaneous
No indication
English
Noniterative finite-difference scheme for modal calculations
British Library Conference Proceedings | 1996
|Modal Testing and Finite Element Calculations for Lightweight Aluminum Panels in Car Carriers
Online Contents | 2006
|