Zobrazeno 1 - 10
of 165
pro vyhledávání: '"Ekaterinaris, J.A."'
Publikováno v:
In Journal of Biomechanics 2 September 2011 44(13):2453-2460
(AIAA Paper 94-0534), Journal of Aircraft, Vol. 32, No. 3, May-Jun. 1995, pp. 625-630. Compressible steady and unsteady flowfields over a NACA 0012 airfoil at transitional Reynolds numbers are investigated. Comparisons with recently obtained experime
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::9e5f203896ef188d1e23a7188b9fd677
https://hdl.handle.net/10945/50074
https://hdl.handle.net/10945/50074
High-order-accurate implicit time-marching methods are presented for discontinuous Galerkin and spectral volume high-order-accurate spatial discretizations of the linearized Euler equations that govern propagation of aeroacoustic disturbances. It is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2127::3ff01ce45807c2c138e8766c3de85bac
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3037283
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3037283
High-order discontinuous Galerkin discretizations for computational aeroacoustics in complex domains
Discontinuous Galerkin discretization is applied for the numerical solution of the linearized Euler equations governing propagation of small-amplitude acoustic disturbances. Second-, fourth-, and sixth-order-accurate numerical solutions are obtained
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https://explore.openaire.eu/search/publication?articleId=od______2127::bd587b4492ac9c5add9f30a0d1f0d4ab
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3037410
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3037410
IUTAM Symposium Transsonicum IV, Ed. Sobieczky., H., Kluwer Academic Publishers, Dordrecht, The Netherlands, 2003, pp. 71-78.< Computational investigations of transonic limit-cycle flutter of the NLR 7301 supercritical airfoil using a thin-layer Navi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::7f27c7340c8c69182b0865ff81960d22
https://hdl.handle.net/10945/37221
https://hdl.handle.net/10945/37221
Autor:
Ekaterinaris, J.A., Platzer, M.F.
Unsteady, separated, high Reynolds number flow over an airfoil undergoing oscillatory motion is investigated numerically. The compressible form of the Reynolds-averaged governing equations is solved using a high-order, upwind biased numerical scheme.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2778::5b10cc3c177250d9cc70f7ec0d38206d
https://hdl.handle.net/10945/50270
https://hdl.handle.net/10945/50270
The analysis and prediction of fluid-structure interaction for viscous, separated flows presents a great challenge to the aeroelastician. In this paper a zonal method for the computation of unsteady, viscous, separated flows over airfoils is presente
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https://explore.openaire.eu/search/publication?articleId=od______2778::6a3b63def2d74a40e8918fb0316945bb
https://hdl.handle.net/10945/50280
https://hdl.handle.net/10945/50280
Proc. of the 5th Asian Congress of Fluid Mechanics, Taejon City, Korea, Aug. 1992, Vol. II, pp. 1047 - 1050.
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https://explore.openaire.eu/search/publication?articleId=od______2778::ef2cfb45c4df164516bc8b378f963f3e
https://hdl.handle.net/10945/50148
https://hdl.handle.net/10945/50148
Experimental and computational investigations of the dynamic stall phenomenon continue to attract the attention of various research groups in the major aeronautical research laboratories. There are two reasons for this continued research interest. Fi
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https://explore.openaire.eu/search/publication?articleId=od______2778::b248b08d349ae1e1d857b62a04b96683
https://hdl.handle.net/10945/60098
https://hdl.handle.net/10945/60098