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An aeroelastic model for composite rotor blades with straight and swept tips. Part I: Aeroelastic stability in hover
Peretz P. Friedmann, Kuo-An Yuan, Marino de TerlizziVolume:
37
Year:
2002
Language:
english
Pages:
20
DOI:
10.1016/s0020-7462(01)00109-3
File:
PDF, 274 KB
english, 2002