Optimal sizing of a composite sandwich fuselage component
Die optimale Dimensionierung eines Flugzeugrumpfs in Sandwichkonstruktion.
Int.J.of Veh.Des. ; 25 , 1/2
2001
26 pages
Int.J.of Veh.Des.;25(2001)1/2 ;89-114
Article (Journal)
English
Optimal sizing of a composite sandwich fuselage component
Online Contents | 2001
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