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An improved technique for testing helicopter rotor-pylon aeromechanical stability using measured rotor dynamic impedance characteristics

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dc.contributor.author Bielawa, R.L.
dc.date.accessioned 2016-07-06T16:41:53Z
dc.date.available 2016-07-06T16:41:53Z
dc.date.issued 1984
dc.identifier.other ERF-1984-097
dc.identifier.uri http://hdl.handle.net/20.500.11881/1457
dc.language.iso en
dc.title An improved technique for testing helicopter rotor-pylon aeromechanical stability using measured rotor dynamic impedance characteristics


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