Contents of volume 13

Composite Structures 13 (1989) 317-318

C O N T E N T S OF V O L U M E 13

Number 1 Impact Response of Tough Carbon Fibre Composites J. MORTON (USA) & E. W. GODWIN (UK) Buckling of Edge-Damaged Filament-Wound Composite Cylindrical Shells under Combined Torsional/Axial Loads. Y. STAVSKY, J. B. GREENBERG & M. SABAG (Israel)

21

Buckling of Thick Layered Composite Plates under In-Plane Moment Loading GAJBIR SINGH, Y. V. K. SADASIVA RAO & N. G. R. IYENGAR (India)

35

Non-destructive Testing of Sandwich Constructions Using Thermography M. VIKSTROM. J. B,~CKLUND & K.-A. OLSSON (Sweden)

49

Computer Aided Design for Composite Structures S. V. HOA, B. H. JOURNEAUX & L. DI LALLA (Canada)

67

Number 2 Recent Studies on the Behaviour of Interference Fit Pins in Composite Plates. T. S. RAMAMURTHY (USA)

81

The Influence of Varying Projectile Mass on the Impact Response of CFRP W. J. CANTWELL & J. MORTON (UK)

101

Correlation between Stress and Strain Based Polynomial Failure Criteria WENCHAO ZHANG & K. E. EVANS (UK)

115

Study on Flexural Vibration of Triangular Composite Plates influenced by Fibre Orientation K. M. LIEW, K. Y. LAM & S. T. CHOW (Singapore) Observations on Bolted Connections in Composite Structures I. H. MARSHALL, W. S. ARNOLD, J. WOOD & R. F. MOUSLEY (UK) Book Reviews

123 133

153 317 Composite Structures (13) (1989)--~ 1989 Elsevier Science Publishers Ltd, England. Printed in Great Britain

31S

(ontents ql Volunle 13 Number .?

Comparison between Shear Deformable and KirchhoffTheories for Bending, Buckling and Vibration of Antisymmetric Angle-ply Laminated Plates . A, A. K l l D E I R (USA)

159

A Study on the Buckling Behavior of an Orthotropic Square Plate with a Central Circular tlole Y. J. LEE, tt. J. L1N& C. C. LIN (Taiwan)

173

Oll the Flexure of Uniform Anisotropic Beams of Rectangular Section J. L. KING (UK) Axisymmetric Stresses in Buried Thin Orthotropic Cylindrical Shells due to P-Wave Loading P. V. M. RAO, V. P. SINGH & P. C. U P A D H Y A Y (India)

183

209

Creep Behaviour of Woven Roving GRP Beam in Three-Point Bending. StlUANG-YIN Z H A N G & BING Z H A O (People's Republic of China)

217

Book Reviews

235 Number 4

Two-Dimensional Orthogonal Polynomials for Vibration of Rectangular Composite Plates K. Y. LAM, K. M. LIEW& S. T. CHOW(Singapore)

239

A Stable Numerical Solution Method for In-plane Loading of NonlinearViscoelastic Laminated Orthotropic Materials K. C. GRAMOLL, D. A. DILLARD & H. F. BRINSON (USA)

251

Thermal Buckling Behavior of Laminated Composite Plates with TemperatureDependent Properties LIEN-WEN CHEN & LEI-YI CHEN (Taiwan)

275

Nonlinear Analysis of Unsymmetrically Laminated Imperfect Thick Panels on Elastic Foundation Y. M. FU & C. Y. CILIA (Canada)

289

Book Reviews

315