Tomblin, J. S., Ng, Y. C., & Raju, K. S. (2001). Material Qualification and Equivalency for Polymer Matrix Composite Material Systems (Report No. DOT/FAA/AR-00/47). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93979
Tomblin, J. S., Y. C. Ng, and K. S. Raju. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems. Report no. DOT/FAA/AR-00/47. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001. https://rosap.ntl.bts.gov/view/dot/93979.
Tomblin, J. S., et al. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001, Report no. DOT/FAA/AR-00/47, ROSA P. https://rosap.ntl.bts.gov/view/dot/93979.
This document presents a qualification plan that will provide the detailed background information and engineering practices to help ensure the control of repeatable base material properties and processes, which are applied to both primary and secondary structures for aircraft products using composite materials. This qualification plan includes recommendations for the original qualification as well as procedures to statistically establish equivalence to the original data set. The plan describes in detail the procedures to generate statistically based design allowables for both A- and B-basis applications. Specific test matrices are presented which produce lamina level composite material properties for various loading modes and environmental conditions for aircraft applications not exceeding 200oF. This plan only covers the initial material qualification at the lamina level and does not include procedures for laminate or higher-level building block tests. The general methodology, however, is applicable to a broader usage.
Tomblin, J. S., Ng, Y. C., & Raju, K. S. (2001). Material Qualification and Equivalency for Polymer Matrix Composite Material Systems (Report No. DOT/FAA/AR-00/47). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/93979
Tomblin, J. S., Y. C. Ng, and K. S. Raju. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems. Report no. DOT/FAA/AR-00/47. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001. https://rosap.ntl.bts.gov/view/dot/93979.
Tomblin, J. S., et al. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 2001, Report no. DOT/FAA/AR-00/47, ROSA P. https://rosap.ntl.bts.gov/view/dot/93979.
ROSA P serves as an archival repository of USDOT-published products including scientific
findings, journal articles, guidelines, recommendations, or other information authored or co-authored by
USDOT or funded partners. As a repository, ROSA P retains documents in their original published format to
ensure public access to scientific information.
Links with this icon indicate that you are leaving a Bureau of Transportation
Statistics (BTS)/National Transportation Library (NTL)
Web-based service.
Thank you for visiting.
You are about to access a non-government link outside of
the U.S. Department of Transportation's National
Transportation Library.
Please note: While links to Web sites outside of DOT are
offered for your convenience, when you exit DOT Web sites,
Federal privacy policy and Section 508 of the Rehabilitation
Act (accessibility requirements) no longer apply. In
addition, DOT does not attest to the accuracy, relevance,
timeliness or completeness of information provided by linked
sites. Linking to a Web site does not constitute an
endorsement by DOT of the sponsors of the site or the
products presented on the site. For more information, please
view DOT's Web site linking policy.
To get back to the page you were previously viewing, click
your Cancel button.