SYMPOSIA PAPER Published: 01 January 1989
STP10357S

Compilation of Procedures for Fatigue Crack Propagation Testing Under Complex Load Sequences

Source

A review is made of procedures, developed at the National Aeronautical Laboratory for fatigue crack propagation testing under flight spectrum loading. They include K-control and on-line spectrum editing that were found to have a significant impact on spectrum load testing. Techniques are described for unambiguous assessment of crack closure stress and for binary-coded marker loading.

Author Information

Sunder, R
National Aeronautical Laboratory, Bangalore, India
Price: $25.00
Contact Sales
Related
Reprints and Permissions
Reprints and copyright permissions can be requested through the
Copyright Clearance Center
Details
Developed by Committee: E08
Pages: 211–230
DOI: 10.1520/STP10357S
ISBN-EB: 978-0-8031-5072-0
ISBN-13: 978-0-8031-1185-1