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Books in the International Committee on Aeronautical Fatigue (ICAF) Series

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	ICAF 14, 1987 - New Materials and Fatigue Resistant Aircraft Design
		€56+€10p&pUK/€20p&pW
		Proceedings of the Fourteenth ICAF (International Committee on Aeronautical Fatigue) Symposium, Ottawa, Canada, June 8-12, 1987 Editor: D. L. Simpson. ISBN 0 947817 29 8 (1987), 629 pages Retail: €116

The Proceedings of the 14th Symposium of The International Committee on Aeronautical Fatigue, 8-12 June, 1987, Ottawa, Canada

CONTENTS

11th PLATEMA MEMORIAL LECTURE

Damage Tolerance in Pressurized Fuselages
T. SWIFT

Fatigue Crack Growth Characterization of Jet Transport Structures
M. MILLER, V. K. LUTHRA and U. GORANSON

Evaluation of New Materials in the Design of Aircraft Structures
M. IOANNOU, L.J. KOK, T.M. FIELDING and N.J. McNEILL

Fatigue of Elevated Temperature Powder Metallurgy Aluminium Alloy Mechanically Fastened Joints
J. C. EKVALL and L.BAKOW

The Fatigue and Corrosion Fatigue Behaviour of Al 7475 T7351 and AL 7091 T7E78 at Low Growth Rates
M. D. RAIZENNE, S. LALONDE, W. WALLACE and I. DICKSON

Microscopic Inner Damage Correlated with Mechanical Property Degradation due to Simulated Fatigue Loading in Metal Matrix Composites
A. KOBAYASHI and N.OHTANI

Fatigue of Evaluation of Mechanically Alloyed Aluminium
W. J. D. SHAW

Aspects of the Fatigue Behaviour of Typical Adhesively Bonded Aircraft Structures
A. GALASSO, A. del CORE, A. LANCIOTTI and L. LAZZERI

Use of Composite Materials to repair Metal Structures
C. A. ELKINS

The Effect of Thickness on Crack Growth Rate
A. NATHAN, D. BENOUALID and A. BROT

Fatigue Crack Propagation Test Program for the A320 Wing
I. G. GRAY

Concise Description and Reconstruction of Spectrum Loading
N. E. DOWLING and S. THANGJITHAM

An Evaluation of a Method of Reconstituting Fatigue Loading from Rainflow Counting
B. H. E. PERRETT

Accounting for Service Environment in the Fatigue Evaluation of Composite Airframe Structure
J. J. GERHARZ, M. BERG and O. GOKGOL

Enstaff a Standard Test Sequence for Composite Components Combining Load and Environment
D.SHUTZ and J. J. GERHARZ

Modelling and Analysis of the effect of "Coldworking" on Fatigue Life
C. AMALBERT, C. CORNUAULT and T. THIBAUD

Damage Tolerance Aspects of an Experimental Arall F-27 Lower Wing Skin Panel
L.H. Van VEGGEL, A.A. JONGEBREUR and J.W. GUNNINK

Consideration of the Early Fatigue Damage on Damage Accumulation and on Delamination Mechanism for Composite Material Structures
V. GIAVOTTO, V. WAGNER, M. CASLINI and C. ZANOTTI

Damage Tolerance of Impact Damaged Carbon Fibre Composite Wing Skin Laminates
T.J. Van BLARICUM, D.S. SAUNDERS, G. CLARK and T.E. PREUSS

Impact and Damage Tolerance Properties of CFRP Sandwich Panels - An Experimental Parameter Study for the Fokker 100 CA - EP Flap
L.H. Van VEGGEL

Certification of Primary Composite Aircraft Structures
R.S. WHITEHEAD

Structural Technology Transition to New Aircraft
J.W. LINCOLN

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