Experimental and Numerical Study of Laminar-Turbulent Transition on a Low-Pressure Turbine Outlet Guide Vane
Journal article, 2021

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CFD

tail bearing housing

821398

engine exit structure

low pressure turbine

turbineexhaust casing

secondaryflow structures

transition

Horizon 2020

European Union (EU)

aerodynamics

CS2-RIA

Clean Sky 2 Joint Undertaking

turbine rear structure

EATEEM

experimental

Author

Isak Jonsson

Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics

Srikanth Deshpande

GKN Aerospace Sweden

Valery Chernoray

Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics

Oskar Thulin

GKN Aerospace Sweden

Jonas Larsson

GKN Aerospace Sweden

Published in

Journal of Turbomachinery

0889-504X (ISSN) 15288900 (eISSN)

Vol. 143 Issue 10 art. no 101011

Research Project(s)

Experimental Aero- and Thermal investigation for a next generation Engine Exit Module (EATEEM)

European Commission (EC) (EC/H2020/821398), 2018-10-01 -- 2021-03-31.

Categorizing

Subject Categories (SSIF 2011)

Aerospace Engineering

Energy Engineering

Fluid Mechanics and Acoustics

Infrastructure

Chalmers Laboratory of Fluids and Thermal Sciences

Identifiers

DOI

10.1115/1.4050629

More information

Latest update

6/3/2022 2