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1-20 of 27
Keywords: turbulence
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Proceedings Papers
Martin Bruschewski, Carolin Wüstenhagen, Clemens Domnick, Robert Krewinkel, Chao-Cheng Shiau, Sven Grundmann, Je-Chin Han
Proc. ASME. GT2022, Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling, V06BT15A005, June 13–17, 2022
Paper No: GT2022-79526
... experimental work cooling systems internal flow CFD data analysis turbulence visualization Abstract Computational Fluid Dynamics (CFD) is the standard tool in the turbomachinery industry to analyze and optimize internal cooling systems of turbine components, but the code applied has...
Proceedings Papers
Proc. ASME. GT2022, Volume 10C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V10CT32A043, June 13–17, 2022
Paper No: GT2022-83376
... at the exit of the prediffuser and the impact that could have on flow split predictions provided to the combustor, Reynold’s stress turbulence models (RSM) are typically used. The combined effort of creating structured meshes, with the difficulty in converging results with RSM can negatively impact design...
Proceedings Papers
Proc. ASME. GT2022, Volume 10D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Turbomachinery General Interest; Unsteady Flows in Turbomachinery, V10DT37A033, June 13–17, 2022
Paper No: GT2022-83497
... motion case is highly unstable, and anisotropic turbulence occurs. The Reynolds stress components are also investigated to show that vortex breakdown and turbulence characteristics. Besides, two typical Reynolds-averaged Navier-Stokes (RANS) models (Sparlat-Allmaras (SA) model and k-ω shear stress...
Proceedings Papers
Proc. ASME. GT2022, Volume 9: Supercritical CO2, V009T28A031, June 13–17, 2022
Paper No: GT2022-83501
... Abstract In order to effectively alleviate the heat transfer deterioration phenomenon of supercritical CO 2 (S-CO 2 ) in a vertical circular tube, explores the fluid hydraulic and thermal performance of multiple turbulator distributed along helices through a verified standard k-ω model...
Proceedings Papers
Stephan Priebe, Daniel Wilkin, II, Andy Breeze-Stringfellow, Arash Mousavi, Rathakrishnan Bhaskaran, Luke d’Aquila
Proc. ASME. GT2022, Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V10AT29A010, June 13–17, 2022
Paper No: GT2022-80683
... Abstract The tip region of transonic blades in turbomachinery involves complex flow physics including shock wave/boundary layer interactions (SBLI). SBLI can lead to flow separation, transition from laminar to turbulent flow, and unsteadiness, which can affect the overall performance...
Proceedings Papers
Proc. ASME. GT2022, Volume 10A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V10AT29A009, June 13–17, 2022
Paper No: GT2022-80538
... Abstract Open rotor fan blades, when exercised across a range of operating conditions and design options, present a variety of complex flow physics including leading-edge flow separation, wake evolution and interaction effects, and laminar-to-turbulent transition. In this paper, we present...
Proceedings Papers
Proc. ASME. GT2022, Volume 6B: Heat Transfer — General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling, V06BT15A021, June 13–17, 2022
Paper No: GT2022-82396
... Abstract The optimal turbulence model to be used in a CFD simulation varies depending on the application and the scientific question at hand. It is always a difficult task to predict which model best represents reality. This study focuses on the internal cooling system of a high-pressure...
Proceedings Papers
Proc. ASME. GT2021, Volume 2A: Turbomachinery — Axial Flow Fan and Compressor Aerodynamics, V02AT31A044, June 7–11, 2021
Paper No: GT2021-60314
... the S groove. The shear matched facility examine the effect of axial casing grooves layers generated as the flows jet out from the upstream ends of (ACGs) geometry on the turbulence in the tip region of an axial the grooves also bring varying elevated turbulence. At BEP, compressor rotor. The ACGs delay...
Proceedings Papers
Proc. ASME. GT2021, Volume 2C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V02CT34A005, June 7–11, 2021
Paper No: GT2021-58711
... Kapilavai Evendale, OH GE Research Niskayuna, NY ABSTRACT Keywords: LES, high-order, wall-resolved, turbine, Engineers performing computational simulations of flow turbulence, aircraft engine, HPC, unstructured grids, GPU physics are often faced with a trade-off between turn-around time and accuracy. High...
Proceedings Papers
Daniel Ferreira Corrêa Barbosa, Daniel da Silva Tonon, Luiz Henrique Lindquist Whitacker, Jesuino Takachi Tomita, Cleverson Bringhenti
Proc. ASME. GT2021, Volume 2C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V02CT34A022, June 7–11, 2021
Paper No: GT2021-59414
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-59414 EVALUATION OF DIFFERENT TURBULENCE MODELS APPLIED IN TURBOPUMP S HYDRAULIC TURBINE Daniel Ferreira Daniel da Silva Tonon Luiz Henrique Jesuino Takachi Corrêa...
Proceedings Papers
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T10A007, September 21–25, 2020
Paper No: GT2020-15229
...EFFECTS OF AXIAL CASING GROOVES ON THE STRUCTURE OF TURBULENCE IN THE TIP REGION OF AN AXIAL TURBOMACHINE ROTOR Huang Chen1, Yuanchao Li1, Subhra Shankha Koley1, Joseph Katz 1* 1 Johns Hopkins University, Department of Mechanical Engineering, Baltimore, MD, USA *katz@jhu.edu ABSTRACT Challenges...
Proceedings Papers
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T10A009, September 21–25, 2020
Paper No: GT2020-15338
...MACHINE LEARNT SYNTHETIC TURBULENCE FOR LES INFLOW CONDITIONS Alessandro Corsini1, Giovanni Delibra1, Marco Giovannelli1, Stefania Traldi1 1Department of Mechanical and Aerospace Engineering Sapienza University of Rome, Italy ABSTRACT LES computations have limited applications in turbomachinery...
Proceedings Papers
Proc. ASME. GT2020, Volume 7B: Heat Transfer, V07BT12A062, September 21–25, 2020
Paper No: GT2020-15830
...Abstract Abstract Large eddy simulations on well-known 7-7-7 fan shaped cooling hole have been carried out. Film cooling methods are generally applied to high pressure turbine, of which flow condition is extremely turbulent because high pressure turbines are generally located downstream...
Proceedings Papers
Proc. ASME. GT2011, Volume 5: Heat Transfer, Parts A and B, 1925-1942, June 6–10, 2011
Paper No: GT2011-46037
.... The findings not only have implications for the vane aerodynamic design, but also for the cooling system design. Keywords: HP NGV, Heat transfer, Combustor Swirl, Aerothermodynamics, Transonic turbine, Vane, Stator, Turbulence. 1 INTRODUCTION Highly swirling flows are now widely employed in gas turbine...
Proceedings Papers
Proc. ASME. GT2009, Volume 2: Combustion, Fuels and Emissions, 657-667, June 8–12, 2009
Paper No: GT2009-59870
... in the time domain based on statistical turbulence quantities. Subsequently, the propagation of the combustion noise is computed by solving the acoustic perturbation equations (APE-4). The accuracy of the RPM-CN approach will be demonstrated by a good agreement of the simulation results with acoustic...
Proceedings Papers
Proc. ASME. GT2008, Volume 3: Combustion, Fuels and Emissions, Parts A and B, 1021-1034, June 9–13, 2008
Paper No: GT2008-51320
... for the reaction rate. The response of the thickened flame to turbulence is taken care of by incorporating an efficiency function in the governing equations. The efficiency function, which is also known as a sub-grid flame wrinkling parameter, is a function of local turbulence and of the premixed flame...
Proceedings Papers
Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1419-1426, June 9–13, 2008
Paper No: GT2008-51340
... is not the same as that commonly used in turbulence models, even when the periodic components are removed from consideration. In particular, the “pseudo-integral-scale”, L ε = q 3 / ε , defined from the turbulence intensity and dissipation, can differ by an order of magnitude or more from the true integral...
Proceedings Papers
Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1313-1322, June 9–13, 2008
Paper No: GT2008-50829
... investigation of the time-averaged mean flow field and turbulence development in an aggressive intermediate turbine duct (downstream a rotating turbine stage) using a 5-hole probe and 2-component hot-wire anemometry. In addition the duct endwall static pressure distribution is discussed. The investigation...
Proceedings Papers
Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 349-363, June 3–6, 2002
Paper No: GT2002-30198
... factors ranged from 25 to 63, preserving the roughness height to boundary layer momentum thickness ratio for each case. The roughness models include samples of deposits, TBC spallation, erosion, and pitting. Measurements were made in a zero pressure gradient turbulent boundary layer at two Reynolds...
Proceedings Papers
Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 75-87, June 3–6, 2002
Paper No: GT2002-30173
... 05 02 2009 The film-cooling performance of a flat plate in the presence of low and high freestream turbulence is investigated using thermochromic liquid crystal thermography. Full-surface distributions of the convective heat transfer coefficient are determined for three blowing rates...