Zobrazeno 1 - 10
of 64
pro vyhledávání: '"P. Reijasse"'
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2020, 234 (1), pp.124-139. ⟨10.1177/0954410018824516⟩
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, SAGE Publications, 2020, 234 (1), pp.124-139. ⟨10.1177/0954410018824516⟩
International audience; An experimental investigation of the transonic flow past the laminar OALT25 airfoil has been conducted to analyze the impact of laminar flow upon the shock wave dynamics and the existence of a laminar buffet like phenomenon. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c18099c221e5b8a667e9fad62b27d97a
https://hal.archives-ouvertes.fr/hal-02612987/document
https://hal.archives-ouvertes.fr/hal-02612987/document
Akademický článek
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Akademický článek
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Autor:
George N. Barakos, D. Stewart, P. Reijasse, Massimo Biava, I. Lipatov, Y. Bondar, Rene Steijl, D. Knight
Publikováno v:
Progress in Flight Physics.
This paper begins by comparing turbulence models for the prediction of hybrid air vehicle (HAV) flows. A 6 : 1 prolate spheroid is employed for validation of the computational fluid dynamics (CFD) method. An analysis of turbulent quantities is presen
Autor:
I. Görgϋlϋ, P. Reijasse, Nermin Ugur, Serkan Özgen, Y. Bondar, D. Knight, Volkan Tatar, I. Lipatov
Publikováno v:
Progress in Flight Physics.
Ice shape predictions for a NACA0012 airfoil and collection efficiency predictions for the Twin Otter airfoil are obtained and presented. The results are validated with reference numerical and experimental data. Ice accretion modeling mainly consists
Publikováno v:
AIAA Journal. 42:2541-2550
Separated flows behind afterbodies in the high subsonic regime are investigated experimentally. Measurements of mean and unsteady wall pressure have been performed in a transonic wind tunnel on axisymmetric configurations with a propulsive jet
Autor:
J.-M. Luyssen, P. Kuszla, S. Palerm, D. Coponet, J.-C. Robinet, J. Oswald, V. Bar, F. Amouroux, P. Reijasse
Publikováno v:
Progress in Propulsion Physics.
A dual-bell nozzle has been tested in the ONERA-R2Ch wind tunnel within the CNES PERSEUS program. The wall pressure distributions and the thrust for the two §ow regimes have been characterized in the nozzle pressure ratio (NPR) range from 51 up to 5
Autor:
P. Reijasse, L. Boccaletto
Publikováno v:
IUTAM Symposium on Unsteady Separated Flows and their Control ISBN: 9781402098970
The influence of the mass flow rate of a film cooling upon the free shock-induced separation inside an over-expanded axisymmetric slot nozzle has been experimentally investigated in the Onera R2Ch wind tunnel. The characteristics of the shock wave -
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f410f38e4ac6c95f61d243e78d550a37
https://doi.org/10.1007/978-1-4020-9898-7_30
https://doi.org/10.1007/978-1-4020-9898-7_30
Publikováno v:
40th AIAA Aerospace Sciences Meeting & Exhibit.