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TASK Quarterly : scientific bulletin of Academic Computer Centre in Gdansk

Tytuł artykułu

Modeling of Rough Wall Boundary Layers with an Intermittency Transport Model

Autorzy Elsner, W.  Warzecha, P. 
Treść / Zawartość
Warianty tytułu
Języki publikacji EN
EN The paper presents a new extension of the -Ret model to account for both the laminar-turbulent transition and the surface roughness. The new modeling approach takes into account the pressure gradient, turbulence intensity and roughness height and density. In the transition region both the intermittency transport equation and the momentum thickness Reynolds number Ret transport equation, supplemented by the correlation of Stripf et al. (2009) suitable for rough wall boundary layers are used. An additional modification of the SST turbulence model allows for modeling a full turbulent boundary layer over surfaces with sand roughness. A comprehensive validation of the new method using transitional and fully turbulent test cases was performed. Flat plate data with a zero and non-zero pressure gradient test case as well as a high pressure turbine blade case were used for this purpose The studies proved that the new modeling approach appeared to be sufficiently precise and enabled a qualitative prediction of the boundary layer development for the tested flow configurations.
Słowa kluczowe
EN surface roughness   boundary layer   turbulence   transition modeling  
Wydawca Centrum Informatyczne Trójmiejskiej Akademickiej Sieci Komputerowej
Czasopismo TASK Quarterly : scientific bulletin of Academic Computer Centre in Gdansk
Rocznik 2010
Tom Vol. 14, No 3
Strony 271--282
Opis fizyczny Bibliogr. 16 poz., rys., tab.
autor Elsner, W.
autor Warzecha, P.
  • Institute of Thermal Machinery, Czestochowa University of Technology, Al. Armii Krajowej 21, 42-200 Częstochowa, Poland,
[1] Waigh D R and Kind R J 1998 AIAA J. 36 (6) 1117
[2] Boynton J L, Tabibzadeh R and Hudson S T 1993 ASME J. Turbomachinery 115 614
[3] Boyle R J and Senyitko R G 2003 ASME Paper, GT-2003-38580
[4] Montomoli F, Hodson H and Haselbach F 2010 ASME J. Turbomachinery 132 31018
[5] Stripf M, Schulz A, Bauer H-J and Wittig S 2009 ASME J. Turbomachinery 131 31017
[6] Bons J P 2010 ASME J. Turbomachinery 132 21004
[7] Aupoix B and Spalart P R 2003 Int. J. Heat and Fluid Flow 24 454
[8] Menter F R, Langtry R B, Likki S R, Suzen Y B, Huang P G and Volker S 2006 J. Turbomachinery 128 413
[9] Piotrowski W, Elsner W and Drobniak S 2010 ASME J. Turbomachinery 132 11020
[10] Medic G and Durbin P A 2002 ASME J. Turbomachinery 124 187
[11] Perry A E, Schofield W H and Joubert P N 1969 J. Fluid Mech. 37 383
[12] Hellsten A and Laine S 1998 AIAA J. 36 (9) 1728
[13] Healzer J M 1974 The Turbulent Boundary Layer on a Rough, Porous Plate: Experimental Heat Transfer with Uniform Blowing, Report HMT-18, Dep. Mech. Eng. Stanford University
[14] Mills A and Hang X 1983 ASME J. Fluids Eng. 105 (3) 364
[15] Coleman H W, Moffat R J and Kays W M 1977 J. Fluid Mech. 82 (3) 507
[16] Zhang X F and Hodson H 2005 ASME J. Turbomachinery 127 479
Kolekcja BazTech
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