AIAA-2006-1862 Nonlinear Flexible Multibody Dynamic Analysis of Rotor Blades with a Trailing Edge Flap
47th, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference ; 2006 ; Newport, R.I
01.01.2006
19 pages
Paper numbers 2006-1600 to 2006-2284 with gaps held
Aufsatz (Konferenz)
Englisch
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Numerical simulation of ice accretion on helicopter rotor blades with trailing edge flap
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