DocumentCode
518444
Title
Notice of Retraction
Parametric study on buckling behavior of composite hat-stiffened panels under uniaxial compression
Author
Zhao Jian ; Xie Zonghong
Author_Institution
Coll. of Astronaut., Northwestern Polytech. Univ., Xi´an, China
Volume
5
fYear
2010
fDate
16-18 April 2010
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Composite stiffened panels are frequently used in aerospace applications. This paper mainly focuses on the buckling behavior of hat stiffened composite panels subjected to uniaxial compression. Parametric analysis model was constructed for typical hat stiffened composite panels through p version finite element approach. Effects of characteristic geometrical parameters on the buckling behavior of hat stiffened composite panels were discussed; several rules and curves were obtained based on the analysis, which will benefit the design of hat stiffened composite panels.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
Composite stiffened panels are frequently used in aerospace applications. This paper mainly focuses on the buckling behavior of hat stiffened composite panels subjected to uniaxial compression. Parametric analysis model was constructed for typical hat stiffened composite panels through p version finite element approach. Effects of characteristic geometrical parameters on the buckling behavior of hat stiffened composite panels were discussed; several rules and curves were obtained based on the analysis, which will benefit the design of hat stiffened composite panels.
Keywords
buckling; composite materials; compressive strength; finite element analysis; structural engineering; structural panels; buckling behavior; composite hat-stiffened panels; finite element method; parametric analysis model; uniaxial compression; Aerospace materials; Composite materials; Educational institutions; Equations; Finite element methods; Geometry; Parametric study; Polynomials; Shape; Stability analysis; buckling; composite; hat stiffened panels; p version; parametric;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-6347-3
Type
conf
DOI
10.1109/ICCET.2010.5486207
Filename
5486207
Link To Document