Vuković, Danijel and Matijašević, Dubravko and Vrdoljak, Milan (2011) Analysis of supersonic flow in Oswatitsch inlet configuration. = Analysis of supersonic flow in Oswatitsch inlet configuration. PAMM : Proceedings in applied mathematics and mechanics, 11 (1). pp. 673-674. ISSN 1617-7061. Vrsta rada: ["eprint_fieldopt_article_type_article" not defined]. . Točan broj autora: 3.
Full text not available from this repository.Abstract
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.
| Item Type: | Article (["eprint_fieldopt_article_type_article" not defined]) |
|---|---|
| Keywords (Croatian): | Oswatitsch inlet, supersonic flow, numerical model of axisymmetric flow |
| Subjects: | TECHNICAL SCIENCE > Aviation, rocket and space technology |
| Divisions: | 1300 Department of Aeronautical Engineering > 1320 Chair of Aircraft Dynamics |
| Date Deposited: | 22 Sep 2016 13:27 |
| Last Modified: | 22 Sep 2016 13:27 |
| URI: | http://repozitorij.fsb.hr/id/eprint/6964 |
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