Residual Strength Pressure Tests and Nonlinear Analyses of Stringer- and Frame-Stiffened Aluminum Fuselage Panels with Longitudinal Cracks
Joint conference; 2nd, Aging aircraft ; 1998 ; Williamsburg; VA
1999-01-01
19 pages
Aufsatz (Konferenz)
Englisch
NASA , aging aircraft , aeronautics , FAA , DoD
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