... passage. In the rough case (fine grid), thick turbulent boundary layers develop along the suction side, and a large recirculation zone is formed downstream of the trailing edge (as shown by the mean Mach number contours in the inset). The wake is fully turbulent and the shedding is highly three...

... for publication in the J ournal of T urbomachinery . 29 07 2024 02 11 2024 04 11 2024 20 12 2024 Graphical Abstract Figure boundary layer development losses turbine aerodynamic design fan compressor and turbine aerodynamic design Engineering and Physical...

... in the U.S. Government’s contributions. 27 07 2024 15 11 2024 18 11 2024 20 12 2024 boundary layer development heat transfer Air Force Research Laboratory 10.13039/100006602 FA8650-21-2-2000 As future aircraft technology is developed, it is expected...

... boundary layer development computational fluid dynamics (CFD) fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines Surface roughness arising through in-service wear and/or the manufacturing process plays a critical role in determining high...

...: 2334325195@qq.com 1 Corresponding author. Email: 724391743@qq.com Email: lehan_lu@163.com Email: 852598003@qq.com 09 04 2024 07 11 2024 07 11 2024 17 12 2024 boundary layer development computational fluid dynamics (CFD) low-pressure turbine flow coefficient...

... urbomachinery . 05 09 2024 11 12 2024 11 12 2024 17 12 2024 Boundary layer development Journal of Turbomachinery. Received September 05, 2024; Accepted manuscript posted December 17, 2024. doi:10.1115/1.4067466 Copyright © 2024 by ASME 1 WAKE - SEPARATION BUBBLE INTERACTION...

... Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the J ournal of T urbomachinery . 18 09 2024 12 12 2024 12 12 2024 17 12 2024 Boundary layer development Measurement techniques turbine blade and measurement advancements Accepted...

... 13 12 2024 Boundary layer development Computational Fluid Dynamics (CFD) fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines Journal of Turbomachinery. Received August 19, 2024; Accepted manuscript posted December 13, 2024. doi:10.1115...

... 12 2024 Boundary layer development Computational Fluid Dynamics (CFD) Fan, compressor, and turbine aerodynamic design fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines Australian Research Council 10.13039/501100000923...

... Figure boundary layer development turbomachinery blading design The increase in fan bypass ratio has been the largest contributor to the increased fuel savings of around 50% [ 1 ] since the introduction of gas turbines in commercial flight. While engine size has been expanding...

.... 121007 . 10.1115/1.4037858 boundary layer development computational fluid dynamics turbomachinery blading design The efficiency and performance of aircraft engines are critical factors influencing overall flight capabilities and fuel consumption. Turbine blades, among the myriad...

... Corresponding author. Emails: jpl@eng.cam.ac.uk ; jpl1000@cam.ac.uk 24 07 2024 23 08 2024 23 08 2024 21 10 2024 boundary layer development measurement techniques surface roughnesss turbine blade and measurement advancements Department for Business, Innovation...

.... Email: stephan.priebe@ge.com 1 Corresponding author. Email: daniel.wilkin@ge.com Email: luke.daquila@ge.com Email: andy.breeze.stringfellow@gmail.com Email: jothipra@ge.com Email: lcheung@sandia.gov boundary layer development computational fluid dynamics (CFD) fan...

... by the ingestion of the boundary layer flow and strong pressure gradients in curved inlet ducts. Therefore improving the characteristics of the ingested flow is one of the main approaches for increasing the submerged inlet performance. boundary layer development computational fluid dynamics (CFD...

... vane of the high-pressure turbine (HPT-NGV). Accurately predicting the heat transfer of the guide vanes is crucial for their mechanical design and the selection of suitable materials. boundary layer development fluid dynamics and heat transfer phenomena in turbine components of gas turbine...

... boundary layer development computational fluid dynamics (CFD) measurement techniques turbomachinery blading design The performance of a turbine is closely related to its internal losses, with up to a third of these losses attributed to secondary flows. These flows primarily arise from...

... layer development computational fluid dynamics (CFD) inter-compressor duct Bundesministerium für Wirtschaft und Energie 10.13039/501100006360 20Q2110C The compression system of most modern civil aircraft engines consists of a fan, a low-pressure compressor (LPC) and a high...

... by the International Gas Turbine Institute (IGTI) of ASME for publication in the J ournal of T urbomachinery . 31 10 2023 23 04 2024 23 04 2024 08 05 2024 Graphical Abstract Figure flow separation boundary layer development compressor stall surge The boundary layer...

... large-eddy simulation boundary layer low pressure turbine secondary flow Reynolds-averaged Navier–Stokes boundary layer development computational fluid dynamics (CFD) fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines Ministerio de...

... developed channel flow and a developing boundary layer. In the channel, Ref. [ 35 ] observed an optimum heat and momentum transfer enhancement at a fixed phase speed. In contrast, in our boundary layer study, the optimal phase speed varies with downstream distance as the boundary layer develops. But despite...