Computational fluid dynamics for turbomachinery internal air systems
Considerable progress in development and application of computational fluid dynamics
(CFD) for aeroengine internal flow systems has been made in recent years. CFD is regularly …
(CFD) for aeroengine internal flow systems has been made in recent years. CFD is regularly …
Achieving high parallel performance for an unstructured unsteady turbomachinery CFD code
N Hills - The aeronautical journal, 2007 - cambridge.org
This paper describes the work done to achieve high parallel performance for an
unstructured, unsteady turbomachinery computational fluid dynamics (CFD) code. The aim …
unstructured, unsteady turbomachinery computational fluid dynamics (CFD) code. The aim …
Building digital twins to simulate manufacturing variation
S Shahpar - Turbo Expo: Power for Land, Sea, and …, 2020 - asmedigitalcollection.asme.org
To improve the quality of a manufactured part in industry, a variety of techniques are used to
scan a built geometry to bring it back to the physics based simulation world to assess its true …
scan a built geometry to bring it back to the physics based simulation world to assess its true …
Development of translucent design philosophy for the cyclic pattern design of Fan outlet guide vanes
D Kulkarni, L di Mare - Journal of Turbomachinery, 2023 - asmedigitalcollection.asme.org
The fan systems of typical high bypass civil engines encounter strong flow distortions
originating in the intake and the bypass duct. These flow distortions cause the fan stage …
originating in the intake and the bypass duct. These flow distortions cause the fan stage …
Compressor/diffuser/combustor aerodynamic interactions in lean module combustors
A Duncan Walker, JF Carrotte, JJ McGuirk - 2008 - asmedigitalcollection.asme.org
The paper reports an experimental investigation into the possibility of increased interactions
between combustor external aerodynamics and upstream components, eg, prediffuser …
between combustor external aerodynamics and upstream components, eg, prediffuser …
Aircraft engine fan tone noise due to back-pressure distortion caused by a downstream pylon under high-speed conditions
S Kusuda, N Yamasaki, C Inoue, M Namba - Journal of Sound and …, 2024 - Elsevier
Experimental, computational fluid dynamics (CFD), and duct-acoustics theoretical studies
were conducted to investigate the mechanism of upstream noise propagation from fan …
were conducted to investigate the mechanism of upstream noise propagation from fan …
Multi-Aeroelastic Phenomena Modelling Part II: Application for the Evaluation of Fan OGV Cyclic Pattern Designs
DY Kulkarni, L di Mare - Turbo Expo: Power for …, 2024 - asmedigitalcollection.asme.org
The cyclic pattern design of fan outlet guide vanes (OGVs) is key to achieving the fan stage
performance and to set the aeromechanical behaviour of low-pressure compressor (LPC) …
performance and to set the aeromechanical behaviour of low-pressure compressor (LPC) …
Attenuation of Inlet Distortion Effects on Fans Using Asymmetric Inlet Guide Vanes
L Liu, HD Vo - Journal of Turbomachinery, 2024 - asmedigitalcollection.asme.org
This research proposes and preliminarily analyzes a novel concept to passively reduce the
negative impact of deep inlet distortion on the fan of an aero-engine. It consists of placing a …
negative impact of deep inlet distortion on the fan of an aero-engine. It consists of placing a …
Fast optimisation of a three-dimensional bypass system using a new aerodynamic design method
F Barbarossa, ME Rife… - … Expo: Power for …, 2017 - asmedigitalcollection.asme.org
The propulsive efficiency of civil aviation power plants can be effectively improved by
increasing the bypass ratio. Higher bypass ratios, however, exacerbate issues of …
increasing the bypass ratio. Higher bypass ratios, however, exacerbate issues of …
Whole turbine CFD modelling
NJ Hills - Turbo Expo: Power for Land, Sea, and Air, 2007 - asmedigitalcollection.asme.org
The level of efficiency of modern turbines means that traditional blade design methods,
based on steady state CFD in an idealised annulus, are no longer able to yield the efficiency …
based on steady state CFD in an idealised annulus, are no longer able to yield the efficiency …