Effects of bidirectional rib arrangements on turbulent flow structure and heat transfer characteristics of a two-pass channel for turbine blade internal cooling

FB Majmader, MJ Hasan - International Communications in Heat and Mass …, 2024 - Elsevier
The thermal efficiency of gas turbine engines depends heavily on the cooling performance
of the internal channels of turbine blades. In the present study, the effects of bidirectionally …

Numerical analysis of heat transfer characteristics in ribbed two-passed channel with varied cross section

M Li, L Luo, S Yang, H Yan, W Du, X Zhou - Physics of Fluids, 2024 - pubs.aip.org
The mid-chord region of turbine blades typically employs internal cooling channels to
enhance heat transfer. However, traditional internal cooling channels are mostly designed in …

Numerical investigation of the flows and heat transfer characteristics of internal cooling channels with separated ribs in gas turbine blades

VH Nguyen, TD Vu, CT Dinh, SG Park - Physics of Fluids, 2024 - pubs.aip.org
Gas turbine engines play a crucial role in numerous industrial domains, including power
generation, aviation, and marine propulsion. One of the major challenges in designing gas …

[PDF][PDF] Heat transfer characteristic of a triangular channel with turbulence promoter

K Takeishi, T Kitamura, M Matsuura… - Proceedings of the …, 2003 - academia.edu
An experimental and analytical study on the heat transfer and pressure loss of a triangular
cooling flow channel with and without turbulent ribs has been conducted for high reliability …

Experimental and numerical investigation of heat transfer characteristics in a square channel with various truncated ribs

J Gong, X Zhang, J Zeng, T Gao, W Wu - Journal of Mechanical Science …, 2019 - Springer
Oblique ribs are widely applied to the internal cooling of turbine blades to promote the heat
transfer between blade wall and coolant. In this study, the effect of several new types of …

Numerical Simulation of Two Pass Gas Turbine Blade Internal Cooling Channels With 90 Degree Varying Height Ribs

S Kumar, RS Amano - … Engineering Congress and …, 2012 - asmedigitalcollection.asme.org
Improvement in thermal efficiency of gas turbine can be obtained by operating it at high inlet
temperatures. In addition to improving the performance, the cons of high inlet temperature is …

Heat transfer and pressure loss in rectangular one-side-ribbed channels with different aspect ratios

S Kunstmann, J Wolfersdorf… - Journal of …, 2013 - asmedigitalcollection.asme.org
An investigation was conducted to assess the thermal performance of W-shaped, 2W-
shaped and 4W-shaped ribs in a rectangular channel. The aspect ratios (W/H) were 2: 1, 4 …

An experimental investigation of the heat transfer in a ribbed triangular cooling channel

M Amro, B Weigand, R Poser, M Schnieder - International Journal of …, 2007 - Elsevier
One of the most challenging aspects of gas turbine cooling is the cooling of the first stages of
turbine blades. Here the highest external heat load is seen at the leading edge of the blade …

Effects of non-uniform wavy ribs on flow and heat transfer characteristics of turbine blade cooling channel

L Wang, C Lv, J Mao, Y Li, D Zhang, X Liu - Applied Thermal Engineering, 2024 - Elsevier
Aiming at the problem of reduced heat transfer performance and uneven distribution along
the ribbed channel in aero-engine turbine blades, the influence mechanism of rib height, rib …

Numerical investigations of pressure loss and heat transfer in a 180 bend of a ribbed two-pass internal cooling channel with engine-similar cross-sections

M Schüler, SO Neumann… - Proceedings of the …, 2010 - journals.sagepub.com
Numerical investigations of a two-pass internal cooling channel with engine representative
cross-sections related to turbine blade cooling were conducted. The channel consisted of a …