Computational fluid dynamics in turbomachinery: a review of state of the art

RN Pinto, A Afzal, LV D'Souza, Z Ansari… - … Methods in Engineering, 2017 - Springer
Computational fluid dynamics (CFD) plays an essential role to analyze fluid flows and heat
transfer situations by using numerical methods. Turbomachines involve internal and external …

A study of fan-distortion interaction within the nasa rotor 67 transonic stage

VJ Fidalgo, CA Hall, Y Colin - 2012 - asmedigitalcollection.asme.org
The performance of a transonic fan operating within nonuniform inlet flow remains a key
concern for the design and operability of a turbofan engine. This paper applies …

Aerodynamics of boundary layer ingesting fans

EJ Gunn, CA Hall - Turbo Expo: Power for Land, Sea …, 2014 - asmedigitalcollection.asme.org
Boundary Layer Ingesting (BLI) turbofan engines could offer reduced fuel burn compared
with podded engines, but the fan stage must be designed to run continuously with severe …

[PDF][PDF] Hydra-CFD: a framework for collaborative CFD development

L Lapworth - … on scientific and engineering computation (IC-SEC), 2004 - researchgate.net
This paper describes a collaborative CFD development framework led by Rolls-Royce plc.
The framework is novel both in the underpinning CFD solver and the network of CFD …

Cloud-based automated design and additive manufacturing: a usage data-enabled paradigm shift

D Lehmhus, T Wuest, S Wellsandt, S Bosse, T Kaihara… - Sensors, 2015 - mdpi.com
Integration of sensors into various kinds of products and machines provides access to in-
depth usage information as basis for product optimization. Presently, this large potential for …

Enhancing the stability of subsonic compressors using casing grooves

T Houghton, I Day - 2011 - asmedigitalcollection.asme.org
Casing grooves are known to increase the stable operating range of axial compressors. The
mechanism by which this stability enhancement occurs is poorly understood. This paper …

Effect of aggressive inlet swirl on heat transfer and aerodynamics in an unshrouded transonic HP turbine

I Qureshi, A Beretta, K Chana, T Povey - 2012 - asmedigitalcollection.asme.org
Swirling flows are now widely being used in modern gas turbine combustors to improve the
combustion characteristics, flame stability, and reduce emissions. Residual swirl at the …

Cokriging for robust design optimization

AJ Keane - AIAA journal, 2012 - arc.aiaa.org
The use of optimization methods to design aerodynamic sections is now completely routine
in many companies and research institutes; see [1] for an introduction to this approach …

Endwall loss in turbine cascades

JD Coull - Journal of Turbomachinery, 2017 - asmedigitalcollection.asme.org
Prior to the detailed design of components, turbomachinery engineers must guide a mean-
line or throughflow design toward an optimum configuration. This process requires a …

The impact of real geometries on three-dimensional separations in compressors

MN Goodhand, RJ Miller - 2012 - asmedigitalcollection.asme.org
This paper considers the effect of small variations in leading edge geometry, leading edge
roughness, leading edge fillet, and blade fillet geometry on the three-dimensional …