Pregled bibliografske jedinice broj: 514744
Analysis of supersonic flow in Oswatitsch inlet configuration
Analysis of supersonic flow in Oswatitsch inlet configuration // PAMM : Proceedings in applied mathematics and mechanics, 11 (2011), 1; 673-674 doi:10.1002/pamm.201110326 (podatak o recenziji nije dostupan, članak, znanstveni)
CROSBI ID: 514744 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Analysis of supersonic flow in Oswatitsch inlet configuration
Autori
Vuković, Danijel ; Matijašević, Dubravko ; Vrdoljak, Milan
Izvornik
PAMM : Proceedings in applied mathematics and mechanics (1617-7061) 11
(2011), 1;
673-674
Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni
Ključne riječi
Oswatitsch inlet; supersonic flow; numerical model of axisymmetric flow
Sažetak
The aim of this work is a study of the flow parameters relevant for the Oswatitsch intake configuration. Geometry of the cone and inlet are equivalent to those on MiG-21bis fighter aircraft. Supersonic flow parameters for a channeled cone were studied at two different operational Mach numbers. Center body cone is movable along longitudinal axis and analysis is focused on specific positions for supersonic flight regimes. To study the problem, numerical model of axisymmetric two-dimensional Euler flow is applied.
Izvorni jezik
Engleski
Znanstvena područja
Zrakoplovstvo, raketna i svemirska tehnika
POVEZANOST RADA
Projekti:
120-1201829-1664 - Numeričke simulacijske procedure dinamike slijetanja elastičnog zrakoplova (Terze, Zdravko, MZOS ) ( CroRIS)
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb
Poveznice na cjeloviti tekst rada:
doi
onlinelibrary.wiley.com
www.wiley-vch.de
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