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Fatigue-crack-propagation and residual-static-strength results on full-scale transport-airplane wings
Author:
Whaley, Richard E.
Additional Authors:
McGuigan, M. J., Jr.
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3847
Link:
https://digital.library.unt.edu/ark:/67531/metadc56105/
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