Computation of unsteady turbomachinery flows: Part 1—Progress and challenges

PG Tucker - Progress in Aerospace Sciences, 2011 - Elsevier
There are numerous unsteady flow influences in turbomachinery. These can potentially
make a substantial total impact on efficiency, and hence the environment and operating …

Trends in turbomachinery turbulence treatments

PG Tucker - Progress in Aerospace Sciences, 2013 - Elsevier
General forms of turbulence models are outlined along with their defects and palliatives for
these in relation to turbomachinery. The turbulence modelling hierarchy available in …

Hierarchical immersed boundary method with smeared geometry

T Cao, P Hield, PG Tucker - Journal of Propulsion and Power, 2017 - arc.aiaa.org
This paper presents a low-order model applying the immersed boundary method on
smeared geometry. It is thus able to represent the effect of turbomachinery within a complex …

[图书][B] Modellierung und Prognose des Grenzschicht-Rotor-Interaktionsschalls für integrierte Triebwerke

M Staggat - 2021 - search.proquest.com
Abstract Das Ziel der vorliegenden Arbeit besteht darin, einen Beitrag zur Bewertung des
Triebwerksschalls bei Flugzeugkonfigurationen mit stark in den Rumpf integrierten …

Effects of boundary-layer ingestion on the aero-acoustics of transonic fan rotors

JJ Defoe, ZS Spakovszky - Journal of …, 2013 - asmedigitalcollection.asme.org
The use of boundary-layer-ingesting, embedded propulsion systems can result in inlet flow
distortions where the interaction of the boundary-layer vorticity and the inlet lip causes …

Assessment of body force methodologies for the analysis of intake-fan aerodynamic interactions

W Thollet, G Dufour… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
With the advent of high bypass ratio turbofan engines of increasing size, new nacelle
designs with shorter air intakes have to be considered, creating new aerodynamic …

Fan similarity model for the fan–intake interaction problem

M Carnevale, F Wang, AB Parry… - … for Gas Turbines …, 2018 - asmedigitalcollection.asme.org
Very high bypass ratio turbofans with large fan tip diameter are an effective way of improving
the propulsive efficiency of civil aero-engines. Such engines, however, require larger and …

Shock propagation and mpt noise from a transonic rotor in nonuniform flow

JJ Defoe, ZS Spakovszky - Journal of …, 2013 - asmedigitalcollection.asme.org
One of the major challenges in high-speed fan stages used in compact, embedded
propulsion systems is inlet distortion noise. A body-force-based approach for the prediction …

Hierarchical geometry modelling using the immersed boundary method

Y Ma, J Cui, NR Vadlamani, P Tucker - Computer Methods in Applied …, 2019 - Elsevier
Abstract The Immersed Boundary Method has been used to simulate a range of fundamental
flows and turbulence. Such studies have demonstrated the method's promising applicability …

Calculation of intake-fan-bypass interaction with a fan similarity model

M Carnevale, F Wang… - … Expo: Power for …, 2018 - asmedigitalcollection.asme.org
Modern trend in installation design is moving towards very high-bypass ratio turbofans. Very
high-bypass turbofans represent an effective way of improving the propulsive efficiency of …