NTL Record

Title Development of Alternating Current Potential Drop (ACPD) Procedures for Crack Detection in Aluminum Aircraft Panels.
Record ID 42256
Personal Name
Creator
Jablonski, David A.
Source 106p. in various pagings
Corporate Creator John A. Volpe National Transportation Systems Center (U.S.)
Publisher United States. Department of Transportation. Federal Aviation Administration
Publication Date 19931201
Language English
Abstract The Alternating Current Potential Drop (ACPD) method is investigated as a means of making measurements in laboratory experiments on the initiation and growth of multiple site damage (MSD) cracks in a common aluminum alloy used for aircraft construction. Procedures for instrumentation MSD test specimens are recommended. The ACPD method is found to be capable of (1) detecting crack initiation at a crack length of the order of 1mm; (2) monitoring crack propagation at a resolution of the order of 5um; and (3) providing an indirect measurement of crack extension in R-curve type tests of fastener hold details.
Public Note Introduction, Experimental procedure, Results and discussion, Summary, Appendices, References
Rosap ID dot:9439
Rosap URL https://rosap.ntl.bts.gov/view/dot/9439
TRT Terms Cracking; Airframes; Mechanical fatigue; Alternating current
General Subjects AC potential drop; Crack growth; Fatigue; R-curve; Inspection; Fracture mechanics; Airframes
Classification NTL - AVIATION - Aviation Safety/Airworthiness
Geographical
Coverage
United States
OCLC 29774858
Report Number DOT-VNTSC-FAA-93-09; DOT-FAA-CT-93-76
Availability Volpe National Transportation Systems Center, Technical Reference Center
Resource type Tech Report
URL https://ntlrepository.blob.core.windows.net/lib/42000/42200/42256/DOT-VNTSC-FAA-93-09.pdf
Format PDF
Database NTL Digital Repository