NASA NTRS · 19810011499
Total main rotor isolation system analysis
Abstract
Requirements, preliminary design, and verification procedures for a total main rotor isolation system at n/rev are presented. The fuselage is isolated from the vibration inducing main rotor at one frequency in all degrees of freedom by four antiresonant isolation units. Effects of parametric variations on isolation system performance are evaluated.
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Sankewitsch, V.. 1981-03-01. Total main rotor isolation system analysis. https://ntrs.nasa.gov/citations/19810011499
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