Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loading
21st Structures, Structural Dynamics, and Materials Conference ; 1980 ; Seattle , WA , U.S.A.
01.01.1980
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
USAF Aircraft Windshield/Canopy Bird Strikes
NTIS | 1983
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