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SEDL / STP / STP1006-EB
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STP1006
Development of Fatigue Loading Spectra
Potter JM, Watanabe RT
Pages: 244
Published: 1989
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Documents the state of the art in characterizing and standardizing cyclic loads experienced by structures in service. From characterizing measured data, to development of standard test spectra. Papers include: Development of Jet Transport Airframe Fatigue Test Spectra, Variable Amplitude Load Models for Fatigue Damage and Crack Growth, and Compilation of Procedures for Fatigue Crack Propagation Testing Under Complex Load Sequences.
Table of Contents
Overview
Potter J., Watanabe R.
Standardized Stress-Time Histories—An Overview
Schütz W.
European Approaches in Standard Spectrum Development
ten Have A.
Development of Jet Transport Airframe Fatigue Test Spectra
Fowler K., Watanabe R.
Basic Approach in the Development of TURBISTAN, a Loading Standard for Fighter Aircraft Engine Disks
Breitkopf G.
Automated Procedure for Creating Flight-by-Flight Spectra
Denyer A.
Progress in the Development of a Wave Action Standard History (WASH) for Fatigue Testing Relevant to Tubular Structures in the North Sea
Dover W., Pook L.
Fatigue Crack Growth in a Rotating Disk Evaluated with the TURBISTAN Mission Spectra
Hoeppner D., Hull D., McCammond D.
Fatigue Spectra Development for Airborne Stores
Fuchs H., Gallagher V., York R.
Simplified Analysis of Helicopter Fatigue Loading Spectra
Dowling N., Khosrovaneh A.
Variable-Amplitude Load Models for Fatigue Damage and Crack Growth
Cornell C., Nelson D., Veers P., Winterstein S.
Tracking Time in Service Histories for Multiaxis Fatigue Problems
Conle F., Oxland T., Topper T., Wurtz D.
Compilation of Procedures for Fatigue Crack Propagation Testing Under Complex Load Sequences
Sunder R.
Author Index
Subject Index
Committee: E08
Paper ID: STP1006-EB
DOI: 10.1520/STP1006-EB
ISBN-EB: 978-0-8031-5072-0
 ASTM International is a member of CrossRef.
0-8031-1185-1
978-0-8031-1185-1
STP1006-EB
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