You are being redirected because this document is part of your ASTM Compass® subscription.
    This document is part of your ASTM Compass® subscription.

    STP1439

    Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions

    McKeighan PC, Ranganathan N
    Published: 2005


      Format Pages Price  
    PDF (14M) $108   ADD TO CART
    Hardcopy (shipping and handling) $108   ADD TO CART
    Hardcopy + PDF Bundle - Save 25%
    (shipping and handling)
    $162.00   ADD TO CART


    Thirty-eight peer-review papers provide the latest information on fatigue testing and analysis under variable amplitude spectrum loading conditions focus purely on fatigue testing, fatigue design techniques, or a combination of both. This new ASTM publication serves as an important reference for engineers and scientists involved in structural integrity and component lifetime management.

    Six sections cover:
    • Fatigue Testing and Laboratory
    • Aerospace Applications, including full-scale aircraft testing
    • Design Approaches and Modelling
    • Other Applications
    • Load Interaction
    • Probabilistic and Multiaxial Effects


    Table of Contents

    Principles of Variable Amplitude Fatigue Design and Testing

    Role of Variable Amplitude Fatigue Standards in Improving Structural Integrity

    A Framework for a Standardization Effort for Fatigue Crack Growth Testing Under Variable Amplitude Spectrum Loading

    Variable Amplitude Fatigue Crack Growth Using Digital Signal Processing Technology

    Variable Amplitude Loading on a Resonance Test Facility

    Development of a DCPD Calibration for Evaluation of Crack Growth in Corner-Notched, Open-Hole Specimens

    The F/A-18E/F Full-Scale Static and Fatigue Test Programs — An Overview

    Spectrum Editing for a Full-Scale Fatigue Test of a Fighter Aircraft Wing with Buffet Loading

    Large Commercial Aircraft Loading Spectra: Overview and State of the Art

    Spectrum Fatigue Testing and Small-Crack Life Prediction Analysis on a Coupon Similar to a Critical Design Detail of a CF188 Hornet Component

    Effect of Transient Loads on Fatigue Crack Growth in Solution Treated and Aged Ti-62222 at -54, 25, and 175°C

    Spectrum Coupon Testing of Fatigue-Resistant Fasteners for an Aging Military Aircraft

    Crack Initiation at a Notch under Constant and Selected Variable Amplitude Loading Conditions

    Fatigue Resistance Evaluation and Crack Kinetics Study for Aero Engine Fan Blades under Random Vibration

    High Cycle Variable Amplitude Fatigue of a Nodular Cast Iron

    Prediction of Crack Growth Under Variable-Amplitude and Spectrum Loading in a Titanium Alloy

    A Model for the Inclusion of Notch Plasticity Effects in Fatigue Crack Growth Analysis

    Comparisons of Analytical Crack Closure Models and Experimental Results Under Flight Spectrum Loading

    Multi-Mechanism Synergy in Variable-Amplitude Fatigue

    Crack Growth and Closure Behavior of Short and Long Fatigue Cracks under Random Loading

    Calculation of Stress Intensity Factors for Cracks in Structural and Mechanical Components Subjected to Complex Stress Fields

    Fatigue Life Modelling and Accelerated Tests for Components under Variable Amplitude Loads

    On the Causes of Deviation from the Palmgren-Miner Rule

    Fatigue Design and Experimentations with Variable Amplitude Loadings in the Automotive Industry

    High Cycle Fatigue Testing and Analysis Using Car Standard Sequence

    Degradation Parameters and Two-Stress Block Fatigue of Angle-Ply Carbon Fiber Reinforced Epoxy

    Study on Fatigue Design Loads for Ships Based on Crack Growth Analysis

    Life Prediction by Observation and Simulation of Short Crack Behavior in a Low Carbon Steel

    Effect of Overloads and Underloads on Fatigue Crack Growth and Interaction Effects

    Overload Effects in Aluminum Alloys: Influence of Plasticity and Environment

    Periodic Overloads in the Near Threshold Regime

    Fatigue Reliability Analysis of an Overload Effect in Welded Joints Including Crack Initiation and Plastic Zone as Random Variables

    Load History in Fatigue: Effect of Strain Amplitude and Loading Path

    Fuzzy Probabilistic Assessment of Aging Aircraft Structures Subjected to Multiple Site Fatigue Damage

    Probabilistic and Semi-Probabilistic Format in Fatigue Ship Classification Rules

    Comparison of the Rain Flow Algorithm and the Spectral Method for Fatigue Life Determination Under Uniaxial and Multiaxial Random Loading

    Validation of Complex Wheel/Hub Subassemblies by Multiaxial Laboratory Tests Using Standardized Load Files

    Fatigue Life of a SG Cast Iron under Real Loading Spectra: Effect of the Correlation Factor Between Bending and Torsion

    Author Index

    Subject Index


    Committee: E08

    DOI: 10.1520/STP1439-EB

    ISBN-EB: 978-0-8031-5503-9

    ISBN-13: 978-0-8031-3479-9

    ASTM International is a member of CrossRef.

    0-8031-3479-7
    978-0-8031-3479-9
    STP1439-EB