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NDT of DC-10 graphite-epoxy rudderThe results of visual and ultrasonic nondestructive tests (NDT) on a DC-10 rudder constructed of Thornel 300/5208 graphite-epoxy are presented. A viscous couplant was used for both contact pulse-echo ultrasonics and the Fokker bondtester. Attention is given to the stiffness of cohesive bond structures (the rudder is assembled primarily in a basic six-ply pattern), and to possible delamination. A piezoelectric transducer is employed to sense changes in impedance and signal amplitude. In all, four rudder units were evaluated. The main problems found in the units were porosity and cracking. It is noted that rudder unit four was able to be sufficiently cured to permit static tests on all rib, spar, and skin panel interfaces.
Document ID
19780051536
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hagemaier, D. J.
(Douglas Aircraft Co. Long Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
May 1, 1978
Publication Information
Publication: Materials Evaluation
Volume: 36
Subject Category
Quality Assurance And Reliability
Accession Number
78A35445
Funding Number(s)
CONTRACT_GRANT: NAS1-12954
Distribution Limits
Public
Copyright
Other

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