Finite Elements in Analysis and Design

Editorial
pp. v-v(1)

Fracture and fatigue analysis of curved or kinked cracks near fastener holes
pp. 91-100(10)
Authors: Chow W.T.; Atluri S.N.

Fracture and fatigue analysis of curved or kinked cracks near fastener holes
pp. 91-100(10)
Authors: W. T.C.; Atluri S.N.

Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints
pp. 101-114(14)
Authors: Deng X.; Hutchinson J.W.

Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints
pp. 101-114(14)
Authors: Xiangyang D.; Hutchinson J.W.

Computational modeling of elastic and plastic multiple cracks by the fundamental solutions
pp. 115-132(18)
Authors: Dong Y.F.; Denda M.

Computational modeling of elastic and plastic multiple cracks by the fundamental solutions
pp. 115-132(18)
Authors: Dong Y.F.; Denda M.

Applications of the three dimensional finite element alternating method
pp. 133-153(21)
Authors: Pipkins D.S.; Atluri S.N.

Applications of the three dimensional finite element alternating method
pp. 133-153(21)
Authors: Pipkins D.S.; Atluri S.N.

Development of a new frame finite element for crash analysis, using a mixed variational principle and rotations as independent variables
pp. 155-171(17)
Authors: Vasudevan S.; Okada H.; Atluri S.N.

Development of a new frame finite element for crash analysis, using a mixed variational principle and rotations as independent variables
pp. 155-171(17)
Authors: Vasudevan S.; Okada H.; Atluri S.N.

Application of metal laminates to aircraft structures: Prediction of penetration performance
pp. 173-192(20)
Authors: Riddle R.; Lesuer D.; Syn C.; Gogolewski R.; Cunningham B.

Application of metal laminates to aircraft structures: Prediction of penetration performance
pp. 173-192(20)
Authors: Riddle R.; Lesuer D.; Syn C.; Gogolewski R.; Cunningham B.

An efficient procedure for determining mixed-mode energy release rates in practical problems of delamination
pp. 193-210(18)
Authors: Davidson B.D.; Hu H.; Yan H.

An efficient procedure for determining mixed-mode energy release rates in practical problems of delamination
pp. 193-210(18)
Authors: Davidson B.D.; Hurang H.; Hongwei Y.

Effects of multiple blade interaction on the containment of blade fragments during a rotor failure
pp. 211-223(13)
Authors: Sarkar S.; Atluri S.N.

Effects of multiple blade interaction on the containment of blade fragments during a rotor failure
pp. 211-223(13)
Authors: Sarkar S.; Atluri S.N.

Hybrid simulation strategy for multiple planar collisions with changing topologies and local deformation
pp. 225-239(15)
Authors: Ogot M.; Liang Y.; Cuitino A.

Hybrid simulation strategy for multiple planar collisions with changing topologies and local deformation
pp. 225-239(15)
Authors: Ogot M.; Y. L.; Cuitino A.

Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires - Part I. Mechanical modeling
pp. 241-263(23)
Authors: Mc Allen J.; Cuitino A.M.; Sernas V.

Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires Part I. Mechanical modeling
pp. 241-263(23)
Authors: Mc Allen J.; Cuitintilde o A.M.; Sernas V.

Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires - Part II. Thermal modeling
pp. 265-290(26)
Authors: Mc Allen J.; Cuitino A.M.; Sernas V.

Numerical investigation of the deformation characteristics and heat generation in pneumatic aircraft tires Part II. Thermal modeling
pp. 265-290(26)
Authors: Mc Allen J.; Cuitintilde o A.M.; Sernas V.

Waves in periodic structures with imperfections
pp. 291-302(12)
Author: Benaroya H.

Waves in periodic structures with imperfections
pp. 291-302(12)
Author: Benaroya H.

Vibration monitoring of cylindrical shells using piezoelectric sensors
pp. 303-318(16)
Authors: Callahan J.; Baruh H.

Vibration monitoring of cylindrical shells using piezoelectric sensors
pp. 303-318(16)
Authors: Callahan J.; Baruh H.

Multiaxial constitutive modeling of aircraft engine materials
pp. 319-332(14)
Authors: Lu Z.K.; Weng G.J.

Multiaxial constitutive modeling of aircraft engine materials
pp. 319-332(14)
Authors: Z. K.L.; G. J.W.

The influence of imperfections on the creep behavior of woven polymer composites at elevated temperatures
pp. 333-347(15)
Authors: Govindarajan S.; Langrana N.A.; Weng G.J.

The influence of imperfections on the creep behavior of woven polymer composites at elevated temperatures
pp. 333-347(15)
Authors: Govindarajan S.; Langrana N.A.; G. J.W.

On the feasibility of using thermal gradients for active control of interlaminar stresses in laminated composites
pp. 349-363(15)
Authors: Kim T.; Steadman D.; Hanagud S.V.; Atluri S.N.

On the feasibility of using thermal gradients for active control of interlaminar stresses in laminated composites
pp. 349-363(15)
Authors: T. K.; Steadman D.; Hanagud S.V.; Atluri S.N.

A systematic design methodology for generating the optimal repairs of aging aircraft
pp. 365-379(15)
Authors: Chickermane H.; Gea H.C.

A systematic design methodology for generating the optimal repairs of aging aircraft
pp. 365-379(15)
Authors: Chickermane H.; Hae C.G.

Integrated decision support for aviation safety inspectors
pp. 381-403(23)
Authors: Luxhoj J.T.; Williams T.P.

Integrated decision support for aviation safety inspectors
pp. 381-403(23)
Authors: Luxhoslashj J.T.; Williams T.P.

Author index volume 23
pp. 405-406(2)

Contents volume 23
pp. 407-408(2)