Design formula for torsional vibration of conically tapered shell fixed at one end and carrying mass of appreciable moment of inertia at free end. (supp)
Fuselage stiffness
Flight
Flight ; 30 , n 1457 ; p 580e-580f
1936
Aufsatz (Zeitschrift)
Englisch
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T-Tail Flutter Analysis with Simulated Fuselage Stiffness
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