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Progressive Damage and Failure Analysis Methods Applications for Aircraft Crashworthiness and Impact Energy ManagementThis report presents a range of analysis methods for performing progressive damage and failure analysis (PDFA) of composite structures with application to crashworthiness analyses and impact event simulation. The report reflects research efforts by the Composite Materials Handbook 17 (CMH–17) Crashworthiness Working Group toward advancing the state of the art in analysis methods and tools. As such, this report serves as a repository of various PDFA methods that users can apply to replicate benchmark problems, incorporating lessons learned to avoid repeating those same errors. Detailed modeling and testing guidelines, along with best practices as the means of compliance subject to regulatory requirements, are deferred to Revision H of CMH–17, Volume 3, Chapter 16, Crashworthiness and Energy Management. The objective of this report is to describe a selection of PDFA methods and show how they are applied in simulating component-level tests involving progressive failure and to present an overall approach for calibrating, evaluating, and validating these PDFA methods. The general intended application of PDFA in this case is aircraft crashworthiness, and therefore the tests are intended to represent aircraft structural features that could be used to manage energy for crashworthiness. Simulation results are compared with flat coupon and C-channel test data for multiple methods, and each of these methods is described in detail, including calibration and material characterization testing requirements. The multiple benefits in using PDFA include the ability to guide testing, reduce design risk, provide response data in support of certification, optimize design features, and perform detailed assessments of structural responses that are difficult to obtain through testing outputs. As with all finite element methods, use of PDFA requires testing for calibration and validation, and test requirements are presented in detail for a range of PDFA methods. Additionally, modeling guidance is provided on strengths, limitations, and recommended practices for several PDFA simulation methods.
Document ID
20250002545
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Mostafa Rassaian
(Boeing Research and Technology Huntington Beach, California)
J Michael Pereira
(Glenn Research Center Cleveland, Ohio, United States)
Alan Byar
(Boeing Impact Simulation Group Everett, Washington, United States)
Aswini Kona Ravi
(National Institute for Aviation Research Wichita, Kansas, United States)
Rudy Haluza
(Pennsylvania State University State College, United States)
Daniel O Adams
(University of Utah Salt Lake City, Utah, United States)
Reza Vaziri
(University of British Columbia Vancouver, Canada)
Johannes Reiner
(University of British Columbia Vancouver, Canada)
Rajaneesh Anantharaju
(GDTech Ans, Belgium)
Matthias Waimer
(German Aerospace Center Stuttgart, Germany)
Thomas Feser
(German Aerospace Center Stuttgart, Germany)
Erin Blessing
(University of Utah Salt Lake City, Utah, United States)
Maria Pia Falaschetti
(University of Bologna Bologna, Italy)
Francesco Rondina
(University of Bologna Bologna, Italy)
Patrick de Luca
(ESI Group (France) Bagneux, France)
Sebastian Müller
(ESI Group (France) Bagneux, France)
Sharon Xiao
(Michigan State University East Lansing, United States)
Juan Pedro Berro Ramirez
(Altair Engineering Inc. Paris, France)
Paolo Feraboli
(Advanced Composite Structures Laboratory Seattle, Washington, United States)
Bonnie Wade
(Advanced Composite Structures Laboratory Seattle, Washington, United States)
Alastair Johnson
(German Aerospace Center Stuttgart, Germany)
Akhil Bhasin
(National Institute for Aviation Research Wichita, Kansas, United States)
Luis Gomez
(National Institute for Aviation Research Wichita, Kansas, United States)
Date Acquired
March 11, 2025
Publication Date
April 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Research and Support Facilities (Air)
Air Transportation and Safety
Report/Patent Number
NASA/TM-20250002545
E-20163
Funding Number(s)
WBS: 664817.02.03.03.03.03
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
External Peer Committee
Keywords
Progressive Damage Analysis
Composite Materials
Aircraft Safety
Crashworthiness
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