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еНаука >  Резултати >  Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime
Title: Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime
Authors Al, Kaabi Hamad; Petrovic, Zlatko; Đukanović, Gordana  
Issue Date: 2019
Publication: Tehnički vjesnik - Strojarski fakultet
ISSN: 1330-3651 Tehnicki Vjesnik = Technical Gazette Search Idenfier
Publisher: Slavonski Brod : Strojarski fakultet.Osijek : Građevinski fakultet.
Type: Article
Collation: vol. 26 br. 3 str. 674-680
DOI: 10.17559/tv-20180724143418
WoS-ID: 000471200400015
Scopus-ID: 2-s2.0-85069738092
VBS COBISS: 514021788
URI: https://enauka.gov.rs/handle/123456789/268466
https://omorika.sfb.bg.ac.rs/handle/123456789/996
https://plus.cobiss.net/cobiss/sr/sr/bib/514021788#izum.si
Metadata source: Migracija
M-category: 
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