NTL Record

Title Testing and analysis of flat and curved panels with multiple cracks
Record ID 50371
Personal Name
Creator
Broek, David; Jeong, David Y.; Thomson, Douglas
Source 14p. in various pagings
Corporate Creator John A. Volpe National Transportation Systems Center (U.S.); Foster-Miller, Inc.
Publisher United States. Department of Transportation. Federal Aviation Administration
Publication Date 19940801
Language English
Abstract An experimental and analytical investigation of multiple cracking in various types of test specimens is described in this paper. The testing phase is comprised of a flat unstiffened panel series and curved stiffened and unstiffened panel series. The test specimens contained various configurations for initial damage. Static loading was applied to these specimens until ultimate failure, while loads and crack propagation were recorded. This data provides the basis for developing and validating methodologies for predicting linkup of multiple cracks, progression to failure, and overall residual strength. The results from twelve flat coupon and ten full scale curved panel tests are presented. In addition, an engineering analysis procedure was developed to predict multiple crack linkup. Reasonable agreement was found between predictions and actual test results for linkup and residual strength for both flat and curved panels. The results indicate that an engineering analysis approach has the potential to quantitatively assess the effect of multiple cracks in the arrest capability of an aircraft fuselage structure.
Rosap ID dot:11759
Rosap URL https://rosap.ntl.bts.gov/view/dot/11759
TRT Terms Aircraft structural components; Cracking; Fatigue cracking; Fuselages; Laboratory tests; Panels; Residual strength; Static loads
Classification NTL - SAFETY AND SECURITY - Vehicle Design;
NTL - SAFETY AND SECURITY - SAFETY AND SECURITY;
NTL - SAFETY AND SECURITY - Aviation Safety/Airworthiness;
NTL - AVIATION - AVIATION;
NTL - AVIATION - Aviation Safety/Airworthiness
Geographical
Coverage
United States
TRIS Online
Accession No
1518859
Resource type Tech Report
URL https://ntlrepository.blob.core.windows.net/lib/50000/50300/50371/19950008046_1995108046.pdf
Alternative URL http://adsabs.harvard.edu/abs/1994asim.nasa...85B
Format PDF
Database NTL Digital Repository