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

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	ICAF 13, 1985 - Durability and Damage Tolerance in Aircraft Design
		€56+€10p&pUK/€20p&pW
		The Proceedings of the Thirteenth ICAF (International Committee on Aeronautical Fatigue) Symposium. Pisa, Italy, May 22-24, 1985. Editors: A. Salvetti and G. Cavallini. ISBN 0 947817 09 3 (1985), 672 pages Retail: $120

The Proceedings of the 13th Symposium of the International Committee on Aeronautical Fatigue, 22 – 24 May, 1985, Pisa, Italy

CONTENTS

Fatigue and Damage Tolerance Work during the Aircraft Design Process
L. JARFALL

Fatigue Life Prediction in the Crack Initiation and Crack Propagation Stages
P. HEULER and W. SCHUTZ

The Significance of Flight-Simulation Fatigue Tests
J. SCHIJVE

Fatigue Life under Compression-Dominated Spectra
R. FRIEDMAN, A. GOMZA, H. ARMEN and H. L. EINDINOFF

Fatigue Cracking of Aluminium under Spectrum Loading at Various Humidities
D. P. CHAPPEL and H. NELSON

Increasing Fatigue and Crack Growth Lives of Short-Edge-Margin Holes
A. BROT and A. NATHAN

Evaluation of Materials Degradation due to Cyclic Loading in Composites
A. KOBAYASHI and N. OHTANI

Damage Tolerance – USAF Experience
J. W. LINCOLN

U. S. Army Requirements for Damage Tolerance of Composite Helicopter Structure
J. P. WALLER and R. S. MCLELLON

Damage Tolerance Test Program of the Fokker 100
A. A. JONGEBREUR, E. PLOUWAARD and R. V. VAN DER VELDEN

Airbus Industrie A310 and A300-600 Experience with Practical Applications of Damage Tolerance Design in Fuselage Primary Structure
H. J. SCHMIDT and C. L. HAMMOND

Continued Airworthiness of Damage Tolerant Aircraft
D. R. TURNER, R. BANISTER and P. TO

Continuing Structural Integrity Program for Transport Aircraft
P. R. ABELKIS, M. B. HARMON and D. S. WARREN

Damage Tolerance and Durability in the Design of a Short-Haul Turboprop Aircraft
A.GALASSO, A. DEL CORE, G. CAVALLINI and A. LANCIOTTI

Maintenance System by Means of Damage Tolerance Principle
K. H. GALDA

A Rationale for the Safe Operation of an Aircraft Fleet having Known Cracks in Primary Structure
J. M. GRANDAGE

The Influence of Slow Growth and Net Section Yielding on the Residual Strength of Stiffened Structure
T. SWIFT

Fracture Diagrams for Stiffened Aircraft Structures: Effects of Material Non-Linearity
M. C. LOW and D. J. CARTWRIGHT

Residual Strength Characterization of Jet Transport Structures
U. G. GORANSON, C. K. GUNTHER and W. T. HARDRATH

A simple Crack Closure Model for Predicting Fatigue Crack Growth under Flight Simulation Loading
D. ALIAGA, A. DAVY and H. SCHAFF

Residual Stress Fields at Notches: Effect on Fatigue Crack Growth
R. COOK and D. P. ROOKE

The Certification of Airframes and Components in Metals and Composite
A. W. CARDRICK

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