NTL Record

Title Full-Scale Testing and Analysis of Curved Aircraft Fuselage Panels.
Record ID 42258
Personal Name
Creator
Samavedam, Gopal; Hoadley, D.; Thompson, D.
Source 48p. in various pagings
Corporate Creator Foster-Miller Associates; 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 report presents data on (1) residual strength of aircraft panels containing Multiple-Site Damage (MSD) in lap splices, and (2) fatigue strength of panels subjected to cyclic pressure loading. The testing was conducted using the dedicated Aging Aircraft Test Facility previously built in the Foster-Miller laboratory. A previous report describes the work in the first phase involving the design and operation of the facility and the test data generated on residual strength of panels with longitudinal midday skin cracks.
Public Note Introduction, Test program, Panel design, Panel residual strength tests, Panel fatigue test, Conclusions and recommendations, References
Rosap ID dot:9440
Rosap URL https://rosap.ntl.bts.gov/view/dot/9440
TRT Terms Airframes; Fuselages; Cracking; Mechanical fatigue; Maintenance
General Subjects Aging aircraft; Multiple-site damage; Fuselage fracture; Fatigue; Lap splice; Residual strength; Maintenance; Airframes
Classification NTL - AVIATION - Aviation Safety/Airworthiness
Geographical
Coverage
United States
OCLC 29786115
Report Number DOT-VNTSC-FAA-93-10; DOT-FAA-CT-93-78
Availability Volpe National Transportation Systems Center, Technical Reference Center
Resource type Tech Report
URL https://ntlrepository.blob.core.windows.net/lib/42000/42200/42258/DOT-VNTSC-FAA-93-10.pdf
Format PDF
Database NTL Digital Repository