Structural health monitoring of a bonded composite patch repair on a fatigue-cracked F-111C wing [el...
Structural health monitoring of a bonded composite patch repair on a fatigue-cracked F-111C wing [electronic resource] / Alan Baker.
About this item
Full title
Author / Creator
Publisher
Fishermans Bend, Victoria : Defence Science and Technology Organisation, 2008.
Date
2008.
Record Identifier
MMS ID
Language
English
Formats
Publication information
Publisher
Fishermans Bend, Victoria : Defence Science and Technology Organisation, 2008.
Place of Publication
Victoria
Date Published
2008.
Access and use
Access Conditions
Commonwealth of Australia 2006.
Subjects
More information
Scope and Contents
Summary
A large fatigue crack in the wing skin of an Australian Defence Force F-111C aircraft was repaired with an adhesively bonded boron/epoxy fibre composite patch. The patch prevented further growth of the crack for 670 flying hours. To aid in the continued safe operation of ADF F-111 aircraft, a decision was later made to assess the residual life of...
Alternative Titles
Full title
Structural health monitoring of a bonded composite patch repair on a fatigue-cracked F-111C wing [electronic resource] / Alan Baker.
Authors, Artists and Contributors
Author / Creator
Notes
General note
Research report / DSTO ; DSTO-RR-0335.
"March 2008"
"AR-014-149"
"DSTO-RR-0335"
Includes bibliographical references.
System details note
Mode of access: Internet via World Wide Web and Adobe Acrobat reader to access the document in PDF format.
Mode of access: Internet via World Wide Web. Available at: http://dspace.dsto.defence.gov.au/dspace/bitstream/1947/9297/1/DSTO-RR-0335%20PR.pdf....
Contextual Information
Other version (online)
Identifiers
Primary Identifiers
Record Identifier
74VvKBRB7Mbl
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/74VvKBRB7Mbl
Other Identifiers
DDC
620.1127
MMS ID
991007956309702626
