STP1439

    Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions

    McKeighan PC, Ranganathan N
    Published: 2005


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    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
    Sonsino C.

    Role of Variable Amplitude Fatigue Standards in Improving Structural Integrity
    Hopkins S., Ménigault J., Mitchell M.

    A Framework for a Standardization Effort for Fatigue Crack Growth Testing Under Variable Amplitude Spectrum Loading
    McKeighan P., McMaster F.

    Variable Amplitude Fatigue Crack Growth Using Digital Signal Processing Technology
    Donald J., George K.

    Variable Amplitude Loading on a Resonance Test Facility
    Hug J., Pöting S., Traupe M., Zenner H.

    Development of a DCPD Calibration for Evaluation of Crack Growth in Corner-Notched, Open-Hole Specimens
    Bucci R., Donald J., George K., Reemsnyder H.

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

    Spectrum Editing for a Full-Scale Fatigue Test of a Fighter Aircraft Wing with Buffet Loading
    Hewitt R., Nor P., Weiss J.

    Large Commercial Aircraft Loading Spectra: Overview and State of the Art
    Beaufils J., Divenah L.

    Spectrum Fatigue Testing and Small-Crack Life Prediction Analysis on a Coupon Similar to a Critical Design Detail of a CF188 Hornet Component
    Everett R., Yanishevsky M.

    Effect of Transient Loads on Fatigue Crack Growth in Solution Treated and Aged Ti-62222 at -54, 25, and 175°C
    Berge S., Glancey C., Lemm D., Stephens R.

    Spectrum Coupon Testing of Fatigue-Resistant Fasteners for an Aging Military Aircraft
    McKeighan P., McMaster F.

    Crack Initiation at a Notch under Constant and Selected Variable Amplitude Loading Conditions
    Gérard N., Girard O., Leroy R., Ranganathan N.

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

    High Cycle Variable Amplitude Fatigue of a Nodular Cast Iron
    Karjalainen-Roikonen P., Marquis G., Rabb B.

    Prediction of Crack Growth Under Variable-Amplitude and Spectrum Loading in a Titanium Alloy
    Newman J., Phillips E.

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

    Comparisons of Analytical Crack Closure Models and Experimental Results Under Flight Spectrum Loading
    Feiger J., McClung R., McMaster F.

    Multi-Mechanism Synergy in Variable-Amplitude Fatigue
    Ashbaugh N., Porter W., Rosenberger A., Sunder R.

    Crack Growth and Closure Behavior of Short and Long Fatigue Cracks under Random Loading
    Kim C., Lee S., Song J.

    Calculation of Stress Intensity Factors for Cracks in Structural and Mechanical Components Subjected to Complex Stress Fields
    Glinka G., Jakubczak H., Nilsson L., Wu Z.

    Fatigue Life Modelling and Accelerated Tests for Components under Variable Amplitude Loads
    Bennebach M., El-Ratal W., Lin X., Plaskitt R.

    On the Causes of Deviation from the Palmgren-Miner Rule
    Endo M., Ishihara S., McEvily A.

    Fatigue Design and Experimentations with Variable Amplitude Loadings in the Automotive Industry
    Bignonnet A., Perroud G., Thomas J.

    High Cycle Fatigue Testing and Analysis Using Car Standard Sequence
    Morel F., Ranganathan N.

    Degradation Parameters and Two-Stress Block Fatigue of Angle-Ply Carbon Fiber Reinforced Epoxy
    Hinz S., Petermann J., Schulte K.

    Study on Fatigue Design Loads for Ships Based on Crack Growth Analysis
    Hashimoto K., Osawa N., Terai K., Tomita Y., Wang Y.

    Life Prediction by Observation and Simulation of Short Crack Behavior in a Low Carbon Steel
    Hünecke J., Schöne D.

    Effect of Overloads and Underloads on Fatigue Crack Growth and Interaction Effects
    de Freitas M., Pommier S., Romeiro F.

    Overload Effects in Aluminum Alloys: Influence of Plasticity and Environment
    Lacroix F., Petit J., Ranganathan N., Tougui A.

    Periodic Overloads in the Near Threshold Regime
    Foulquier J., Pippan R., Rapaport A., Sereni S., Tabernig B.

    Fatigue Reliability Analysis of an Overload Effect in Welded Joints Including Crack Initiation and Plastic Zone as Random Variables
    Darcis P., Recho N.

    Load History in Fatigue: Effect of Strain Amplitude and Loading Path
    Aubin V., Degallaix S., Quaegebeur P.

    Fuzzy Probabilistic Assessment of Aging Aircraft Structures Subjected to Multiple Site Fatigue Damage
    Akpan U., Dunbar T., Koko T., Rushton P.

    Probabilistic and Semi-Probabilistic Format in Fatigue Ship Classification Rules
    Césarine G., Huther M., Mahérault S., Parmentier G.

    Comparison of the Rain Flow Algorithm and the Spectral Method for Fatigue Life Determination Under Uniaxial and Multiaxial Random Loading
    Łagoda T., Macha E., Niesłony A.

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

    Fatigue Life of a SG Cast Iron under Real Loading Spectra: Effect of the Correlation Factor Between Bending and Torsion
    Banvillet A., Palin-Luc T., Vittori J.

    Author Index

    Subject Index


    Committee: E08

    Paper ID: STP1439-EB

    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