A method for predicting the aerodynamic loads and dynamic response of the rotor blades of a tandem-rotor helicopter.


Autoria(s): Balcerak, John C.
Data(s)

31/12/1969

Resumo

"USAAVLABS technical report 67-38."

Mode of access: Internet.

Formato

bib

Identificador

http://hdl.handle.net/2027/coo.31924004631093

Idioma(s)

eng

Publicador

Ft. Eustis, Va., U.S. Army Aviation Materiel Laboratories

Direitos

Items in this record are available as Public Domain, Google-digitized. View access and use profile at http://www.hathitrust.org/access_use#pd-google. Please see individual items for rights and use statements.

Palavras-Chave #Rotors (Helicopters)
Tipo

text