Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Jan Windte"'
Autor:
Jan Windte, Rolf Radespiel
Publikováno v:
AIAA Journal. 46:2165-2177
Unsteady Reynolds-averaged Navier-Stokes simulations of the low-Reynolds-number flow past an SD7003 airfoil with combined plunge and pitch motion at Re=60, 000 are presented in which transition takes place across laminar separation bubbles. The numer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2eeed6ee35f3925370723db9f7aaa515
https://doi.org/10.2514/1.30569
https://doi.org/10.2514/1.30569
Publikováno v:
The Aeronautical Journal. 111:17-29
This paper presents investigations of low-Reynolds-number flows past an SD7003 aerofoil at Re = 60k, where transition takes place across a laminar separation bubble (LSB). Results of experimental measurements and numerical calculations are analysed a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::839a2fbac5f3c037cd2f9a8df5db5fec
https://doi.org/10.1017/s000192400000172x
https://doi.org/10.1017/s000192400000172x
Publikováno v:
Aerospace Science and Technology. 10:484-494
This paper presents RANS simulations of the low-Reynolds-number flow past an SD7003 airfoil at Re = 6 × 10 4 , where transition takes place across a laminar separation bubble. The transition prediction procedure using an approximate envelope method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a1928a80a3d5e05de1f4bfc9de146a8a
https://doi.org/10.1016/j.ast.2006.03.008
https://doi.org/10.1016/j.ast.2006.03.008
Publikováno v:
28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
The present work describes particle image velocimetry at M = 5.9 in the Hypersonic Ludwieg Tube Braunschweig on a generic space launcher model. The wind tunnel allows high quality flows as well as high repetition rates and, thus, it is suited for PIV
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d808e676d57dd5f3f87fb415be919ddf
https://doi.org/10.2514/6.2012-3197
https://doi.org/10.2514/6.2012-3197
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
To investigate the aeroelastic eects, the design as well as the numerical analysis of a flexible and oscillating airfoil is described in this contribution. Due to the interaction of the fluid flow with the structural system, a multiphysical approach
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::670ea00b32fa1161078832c8887510b4
https://doi.org/10.2514/6.2008-306
https://doi.org/10.2514/6.2008-306
Publikováno v:
MEGAFLOW-Numerical Flow Simulation for Aircraft Design ISBN: 9783540243830
The laminar flow around a NACA 4402 airfoil is investigated at a Reynolds number of Re = 6000 using the RANS solver FLOWer. Significant flow separation occurs over almost the whole regime of angles of attack for steady onset flow conditions. Therefor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f158d1e602f529e0b511ec07f6f8193
https://doi.org/10.1007/3-540-32382-1_21
https://doi.org/10.1007/3-540-32382-1_21
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
Experimental measurements and unsteady Reynolds-averaged Navier-Stokes simulations of the low-Reynolds-number flow past an SD7003 airfoil with and without plunge motion at Re = 60 k are presented, where transition takes place across laminar separatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c0556bc919c0f8bf5d9b3ce4643bd32d
https://doi.org/10.2514/6.2006-501
https://doi.org/10.2514/6.2006-501
Publikováno v:
23rd AIAA Applied Aerodynamics Conference.
This paper presents an investigation of low-Reynolds-number flows past an SD7003 airfoil at Re = 60K, where transition takes place across a laminar separation bubble (LSB). Results of experimental measurements and numerical calculations are analyzed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b9805445a0e6ebaa7ef5045fc748979
https://doi.org/10.2514/6.2005-4607
https://doi.org/10.2514/6.2005-4607
Publikováno v:
Scopus-Elsevier
Nomenclature A = calibration matrix c = chord length of the airfoil cl = lift coefficient f = frequency of the flapping stroke fobjective = focal length of the camera objective k = reduced frequency lϕ = amplitude of the periodic sliding carriage mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7cb61e04665ecd2c05d366860104a385
http://www.scopus.com/inward/record.url?eid=2-s2.0-78149457943&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-78149457943&partnerID=MN8TOARS