Internal report (Reports)
Moderate deflection analysis of shelles of revolution, using cylindrical components of the displacement
Debongnie, Jean-François
1984
 

Files


Full Text
LMF-D6.pdf
Author postprint (748.24 kB)
Download

All documents in ORBi are protected by a user license.

Send to



Details



Keywords :
Shell theory; Moderate deflections; Rigid body motions
Abstract :
[en] This paper is devoted to the analysis of shells of revolution, using cylindrical components of the displacement. This procedure, as coupled with a Fourier expansion by respect of the azimuth, permits the generation of finite elements in which rigid body are represented exactly, even in the case of doubly curved shells.
Research Center/Unit :
Ecole Mohammadia d'Ingénieurs, Rabat, Marocco
Disciplines :
Mechanical engineering
Author, co-author :
Debongnie, Jean-François ;  Université de Liège - ULiège > Département d'aérospatiale et mécanique > Méthodes de fabrication
Language :
English
Title :
Moderate deflection analysis of shelles of revolution, using cylindrical components of the displacement
Alternative titles :
[fr] Analyse des déflexions modérées des coques de révolution, en utilisant les composantes cylindriques des déplacements
Publication date :
September 1984
Report number :
LMF/D6
Number of pages :
17
Available on ORBi :
since 10 July 2009

Statistics


Number of views
83 (4 by ULiège)
Number of downloads
45 (2 by ULiège)

Bibliography


Similar publications



Sorry the service is unavailable at the moment. Please try again later.
Contact ORBi