Loads in a fuselage under combined bending and torsion
1933
30, [2] S.
graph. Darst.
Auch u.d.T.: The influence of end fixing conditions and of bulkhead wires upon the loads in the members of an aeroplane fuselage under combined bending and torsion
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
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