OPTIMAL WEIGHT DESIGN OF LAMINATED COMPOSITE PANELS WITH DIFFERENT STIFFENERS UNDER BUCKLING LOADS
Congress; 27th, International Council of the Aeronautical Sciences (Congress); ICAS 2010; [electronic resource] ; 2010 ; Nice, France
International Council of the Aeronautical Sciences (Congress); ICAS 2010; [electronic resource] ; ICAS 2010-8.9.1
2010-01-01
ICAS 2010-8.9.1
Includes bibliographical references and author index; Held on CD-ROM
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Buckling Analysis of Geodesically Stiffened Composite Panels with Discrete Stiffeners
Online Contents | 1994
|Thermomechanical Buckling and postbuckling Responses Composite Panels with Skewed Stiffeners
British Library Conference Proceedings | 1996
|