Stiffened 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.


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    Title :

    Fatigue and residual strength investigation of ARALL(R) -3 and GLARE(R) -2 panels with bonded stringers


    Contributors:
    Wu, Ming (author) / Wilson, Dale A. (author) / Reddy, S. V. (author)


    Publication date :

    1994-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Fatigue and Residual Strength Investigation of Arall[R]-3 and Glare[R]-2 Panels with Bonded Stringers

    Wu, M. / Wilson, D. A. / Reddy, S. V. et al. | British Library Conference Proceedings | 1994


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