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Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions
Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions
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Mathematical modeling of Ka-226 Ka-26 helicopter.pdf
(1.23 MB)
Date
2007
Authors
Burtsev, B.N.
Ryabov, V.I.
Selemenev, S.V.
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http://hdl.handle.net/20.500.11881/221
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