ICAF 16, 1991 - Aeronautical Fatigue: Key to Safety and Structural Integrity

ICAF 16, 1991 – Aeronautical Fatigue: Key to Safety and Structural Integrity

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Proceedings of the Sixteenth ICAF (International Committee on Aeronautical Fatigue) Symposium, Tokyo, Japan, May 22-24, 1991 Editor: A. Kobayashi.
ISBN 4 9900181 1 7 (1991), 492 pages Retail: €160 .

SKU: ISBN 4 9900181 1 7

The Proceedings of the 16th Symposium of the International Committee on Aeronautical Fatigue, 22-24 May, 1991, Tokyo, Japan

CONTENTS

13th PLATEMA MEMORIAL LECTURE

Structural Integrity Challenges
R. M. BADER

Aircraft Tracking Optimization of Parameters Selection
R.J. CAZES and P. DEFOSSE

Loads at the Nose Landing Gears of Civil Transport Aircraft During Towbarless Towing Operations
O. BUXBAUM, J. J. CUNY, H. KLATSCHKE and H. STEINHILBER

New Lamps for Old Safety Regulations through Structural Airworthiness Standards
A. J. EMMERSON

Reassessment of the C-141 Structural Life
J. W. LINCOLN

Maintaining the Safety of an Aging Fleet of Aircraft
A. W. HOGGARD

Fleet Fatigue Cracking Threshold Prediction
I. C. WHITTAKER, P. B. STILWELL and D. R. SIZEMORE

A Review of Aging Aircraft Technology – an I. A. I. Perspective
A. BROT and A. NATHAN

Aging Review of the YS-11 Aircraft
T.SHIOHARA, M. NAKATA and H. KUMADA

Super Puma MK II : Rotor and Gearbox Fatigue
G. MESNARD

The Role of Fatigue Testing in the Design, Development and Certification of the ATR 42/72
A. MINUTO, S. SCAFARO, A. LANCIOTTI and L. LAZZERI

Aging Aircraft, Detection of Multiple Site Damage, and the Risk of Failure
P. TONG, S. G. SASMPATH and D. BROEK

Analysis of Multiple Crack Propagation in Stiffened Sheet
H. -P. LEHRKE and A. SCHOPFEL

Bulging of Fatigue Crack in a Pressurized Aircraft Fuselage
D. CHEN and J. SCHIJVE

Effects of Prior Fatigue Damage on Crack Propagation Rates in 2024-T351 Aluminium Alloy
W. J. D. SHAW

Interpretation of Fatigue Crack Growth Test Data for Damage Tolerance Analysis
M. OORE

Damage Tolerance Assessment on the Multi-Size Cracks for the YS-11 Aircraft
M. NAKATA, T. NISHIMURA and K. INABA

Damage Tolerant Aluminium-Lithium Alloy 8090 Sheet
D. S. McDARMAID, G. R. SUTTON, C. WHEELER, C. E. THOMAS, C. J. PEEL and R. N. WILSON

Flight Simulation and Constant Amplitude Fatigue Crack Growth in Aluminium-Lithium Sheet and Plate
R. J. H. WANHILL, W. G. J. T. HART and L. SCHRA

Fatigue Life Prediction for Carbon-Epoxy Composite Design
B. D. WRIGHT

Fatigue Qualification of High Thickness Composite Rotor Components
M. RAGGI, U. MARIANI and G. ZAFFARONI

List of Attendees to the 1991 ICAF Meeting