Evaluation of an aluminum fuselage panel with discrete-source damage and subjected to combined loading conditions
40th Structures, Structural Dynamics, and Materials Conference and Exhibit ; 1999 ; St. Louis , MO , U.S.A.
01.01.1999
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Design and Evaluation of Composite Fuselage Panels Subjected to Combined Loading Conditions
British Library Conference Proceedings | 1998
|Design and Evaluation of Composite Fuselage Panels Subjected to Combined Loading Conditions
Online Contents | 2005
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