|
|
|
SEDL / STP / STP1439-EB
 |
STP1439
Fatigue Testing and Analysis Under Variable Amplitude Loading Conditions
McKeighan PC, Ranganathan N
Pages: 582
Published: 2005
|
|
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
ASTM International is a member of CrossRef.
0-8031-3479-7
978-0-8031-3479-9
STP1439-EB
|