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Digital Library / STP / STP1006-EB
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Development of Fatigue Loading Spectra
Potter JM
Pages: 244
Published: 1989
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Description
Table of Contents
Overview
Potter JM, Watanabe RT
Standardized Stress-Time HistoriesAn Overview
Schütz W
European Approaches in Standard Spectrum Development
ten Have AA
Development of Jet Transport Airframe Fatigue Test Spectra
Fowler KR, Watanabe RT
Basic Approach in the Development of TURBISTAN, a Loading Standard for Fighter Aircraft Engine Disks
Breitkopf GE
Automated Procedure for Creating Flight-by-Flight Spectra
Denyer AG
Progress in the Development of a Wave Action Standard History (WASH) for Fatigue Testing Relevant to Tubular Structures in the North Sea
Pook LP, Dover WD
Fatigue Crack Growth in a Rotating Disk Evaluated with the TURBISTAN Mission Spectra
Hull DA, McCammond D, Hoeppner DW
Fatigue Spectra Development for Airborne Stores
Gallagher VM, York RL, Fuchs HO
Simplified Analysis of Helicopter Fatigue Loading Spectra
Dowling NE, Khosrovaneh AK
Variable-Amplitude Load Models for Fatigue Damage and Crack Growth
Veers PS, Winterstein SR, Nelson DV, Cornell CA
Tracking Time in Service Histories for Multiaxis Fatigue Problems
Conle FA, Oxland TR, Wurtz D, Topper TH
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
ASTM International is a member of CrossRef.
0-8031-1185-1
978-0-8031-1185-1
STP1006-EB
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