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eNauka >  Results >  Numerical evaluation of the aerodynamic influence of the helicopter composite blade trailing edge tabs
Title: Numerical evaluation of the aerodynamic influence of the helicopter composite blade trailing edge tabs
Authors: Kostić, Ivan  
Issue Date: 2007
Publication: Archive of Applied Mechanics
ISSN: 0939-1533 Archive of Applied Mechanics Search Idenfier
Publisher: Springer, New York
Type: Article
Collation: vol. 77 br. 12 str. 893-909
DOI: 10.1007/s00419-007-0133-1
WoS-ID: 000250137900004
Scopus-ID: 2-s2.0-35348895577
URI: https://machinery.mas.bg.ac.rs/handle/123456789/707
https://enauka.gov.rs/handle/123456789/567887
M-category: 
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