NASA NTRS · 19810018538
Total main rotor isolation system analysis
Abstract
The requirements for a preliminary design study and verification procedure for a total main rotor isolation system at n/rev are established. The system is developed and analyzed, and predesign drawings are created for an isolation system that achieves over 95 percent isolation of all six degrees of freedom.
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Halwes, D. R.. 1981-06-01. Total main rotor isolation system analysis. https://ntrs.nasa.gov/citations/19810018538
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