Keywords: Laminates
Close
Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2009) 81 (3): 221–225.
Published: 15 May 2009
...Timothy C. Kennedy; Sergio G. Arias Purpose The purpose of this paper is to determine the validity of using classical laminated plate theory to predict strain concentration factors in notched laminates under bending. Design/methodology/approach The objective was accomplished by comparing...
Journal Articles
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (6): 486–490.
Published: 01 December 2005
.... The study is focused upon long, intermediate and short cylindrical shells as defined by Aas‐Jakobsen's parameters and considers symmetric and unsymmetric composite laminates. Findings The non‐dimensional fundamental natural frequencies are obtained for angle ply (45/−45/45, 45/−45) and cross ply (0/90/0...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2005) 77 (1): 52–61.
Published: 01 February 2005
... load is gradually decreasing with the increasing cut‐out size; load bandwidth and type of load conditions have significant influence on flutter and divergence characteristics of both isotropic and laminated curved panels; damping is perceived to have significant effect on flutter behaviour; the effect...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2004) 76 (4): 404–413.
Published: 01 August 2004
... failure under bone dry and hygrothermal environments. The behaviour of such joints is complex due to the geometry of the joint configuration and laminated construction. T‐joints are also susceptible when exposed to moisture and temperature environments. As a consequence, the stiffness and strength...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2004) 76 (1): 29–37.
Published: 01 February 2004
...Anup Ghosh; P.K. Sinha In the present investigation, a finite element analysis procedure is developed to predict the initiation and propagation of damages as well as to analyse damaged laminated composite plates under forced vibration and impact loads. Isoparametric quadratic plate bending element...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (6): 558–570.
Published: 01 December 1999
...A. Vlot; L.B. Vogelesang; T.J. de Vries Fibre metal laminates were developed at Delft University during the last two decades as a family of new hybrid materials consisting of bonded thin metal sheets and fibre/adhesive layers. This laminated structure provides the material with excellent fatigue...
Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (1999) 71 (1)
Published: 01 February 1999
... approach would be to machine the master model from polyurethane modelling board directly from the CAD surface geometry. Cibatool takes to the air! Keywords Aircraft,Ciba, Laminates British Aerospace Regional Aircraft Ltd, Prestwick, chose Cibatool BM5460 Polyurethane Tooling Board in its...

or Create an Account

Close Modal
Close Modal