It is assumed that pure antisymmetric vibrations can exist, involving fuselage torsion but excluding fuselage bending; with this assumption, eigenvalue equations for anti-symmetric vibrations of complete aircraft are derived in very general form.
Anti-symmetric vibrations of aircraft
Aeronautical Quarterly
Aeronautical Quarterly ; 3 , Part 2
1951
16 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1944
|Emerald Group Publishing | 1944
|Emerald Group Publishing | 1944
|Emerald Group Publishing | 1944
|Emerald Group Publishing | 1944
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