A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter.
Data(s) |
31/12/1969
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Resumo |
"USAAVLABS technical report 67-38." Mode of access: Internet. |
Formato |
bib |
Identificador | |
Idioma(s) |
eng |
Publicador |
Ft. Eustis, Va., U.S. Army Aviation Materiel Laboratories |
Direitos |
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Palavras-Chave | #Rotors (Helicopters) |
Tipo |
text |