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

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ICAF 15, 1989 - Aeronautical Fatigue in the Electronic Era

  ICAF 15

€56+€10p&pUK/€20p&pW

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Proceedings of the Fifteenth ICAF (International Committee on Aeronautical Fatigue) Symposium, Jerusalem, Israel, June 21-23, 1989. Editor: A. Berkovits. ISBN 0 947817 35 2 (1989), 545 pages
Retail: $140

Proceedings of the 15th Symposium of the International Committee On Aeronautical Fatigue 21-23 June, 1989, Jerusalem, Israel

CONTENTS

12th PLATEMA MEMORIAL LECTURE

Assessment of Service Load Experience
J.B. de JONGE

Description and Reconstitution of Manoeuvre Loadings
O.BUXBAUM and H. STEINHILBER

The Operational Loads Monitoring System (OLMS)
H. -J.MEYER and V. LADDA

Tracking B-1B Aircraft with a Structural Data Recorder
A.G. DENYER

Verification of Loads, Fatigue Performance and Damage Tolerance of the JA39 Gripen
L.JARFALL

Re-Assessing the F-16 Damage Tolerance and Durability Life of the RNLAFF- 16 Aircraft
D.J. SPIEKHOUT

Eight Years of Experience with Small Computerized Retrofit Load Monitoring Systems
B. BRUNNER and R. KAESER

The Survivability of Centrifugal Compressors in Modern Aircraft Engines
K. N. SHOHET and R. N. TADROS

A Rate Theory Investigation of Cyclic Loading and Plastic Deformation in the High Stress and Ambient Temperature Range
A. S. KRAUSZ, Z. W. LIAN, J. S. MSHANA and K. KRAUSZ

Fractographic Techniques for the Assessment of Aircraft Component Cracking
N.T. GOLDSMITH and G. CLARK

Acoustic Fatigue Analysis by the Finite Element Method
Z. H. GRANOT

The Use of Modern Fastening Systems to Enhance the Fatigue Life of Thin Sheet Structure
A. SIMPSON

Damage Tolerance for Helicopters
J. W. LINCOLN

Douglas Aging Aircraft Programs
J. A. McGREW and A. W. HOGGARD

Ageing Jet Transport Structural Evaluation Programs
U.G. GORANSON and M. MILLER

Development of a Double Crack Growth Gage Algorithm for Application to Fleet Tracking of Fatigue Damage
A. DUMANIS and A.F. GRANDT Jr

Application of the “K-Gage” to Aircraft Structural Testing
S. MIYAKE, Y. NAWA, Y. KONDO and T. ENDO

A Probabilistic Approach for the Establishment of an Aircraft Structure Inspection Program
A. ALBIN, L. GRANDPIERRE and B. HECIAK

Understanding Composite Fatigue: New Trends
V. GIAVOTTO, C. CAPRILE and S.SALA

Damage Tolerance Demonstration for A310 – 300 CFRP Components
O. GOKOL

Probabilistic Approach to the Certification for Fatigue Durability of Composite Structures
T. SHIMOKAWA

Impact Damage in Fatigue Loaded Composite Structures
J. J. GERHARZ, H. IDELBERGER and H. HUTH

In-Service Detection of Impact Damage in Composite Materials
J. H. HEIDA

 

 

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