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                                       Details for article 23 of 46 found articles
 
 
  Impact of the fuselage damping characteristics and the blade rigidity on the stability of helicopter
 
 
Title: Impact of the fuselage damping characteristics and the blade rigidity on the stability of helicopter
Author: Chellil, A.
Nour, A.
Lecheb, S.
Kebir, H.
Chevalier, Y.
Appeared in: Aerospace science and technology
Paging: Volume 29 (2013) nr. 1 pages 18 p.
Year: 2013
Contents:
Publisher: Elsevier Masson SAS
Source file: Elektronische Wetenschappelijke Tijdschriften
 
 

                             Details for article 23 of 46 found articles
 
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