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Fatigue and residual strength investigation of ARALL(R) -3 and GLARE(R) -2 panels with bonded stringersStiffened panels were fabricated from ARALL-3 and GLARE-3 laminates for the purpose of providing improved structural performance of lower wing panels for aircraft. To verify the designs fatigue crack growth and residual strength tests were conducted and compared to those for conventional monolithic aluminum panels.
Document ID
19950013079
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wu, Ming (Tennessee Technological Univ. Cookeville, TN, United States)
Wilson, Dale A. (Tennessee Technological Univ. Cookeville, TN, United States)
Reddy, S. V. (Textron Aerostructures Nashville, TN., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA. Langley Research Center, FAA(NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, Part 2
Subject Category
Aircraft Design, Testing And Performance
Accession Number
95N19495
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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