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 …

Analysis of fan stage conceptual design attributes for boundary layer ingestion

DK Hall, EM Greitzer, CS Tan - Journal of …, 2017 - asmedigitalcollection.asme.org
This paper describes a new conceptual framework for three-dimensional turbomachinery
flow analysis and its use to assess fan stage attributes for mitigating adverse effects of inlet …

[HTML][HTML] Advanced low-noise aircraft configurations and their assessment: past, present, and future

ZS Spakovszky - CEAS Aeronautical Journal, 2019 - Springer
Aircraft noise remains the key inhibitor of the growth of air transportation, but the focus of the
noise mitigation strategies has changed. As the propulsor fan pressure ratio is decreased for …

[HTML][HTML] Numerical analysis of fan noise for the NOVA boundary-layer ingestion configuration

G Romani, Q Ye, F Avallone, D Ragni… - Aerospace Science and …, 2020 - Elsevier
Aim of this paper is to investigate the effects of the turbulent flow developing over a fuselage
on fan noise for BLI embedded propulsion systems. Such configurations can suffer from inlet …

Inlet flow distortion in an advanced civil transport boundary layer ingesting engine installation

DK Hall, EM Greitzer, A Uranga… - Journal of …, 2022 - asmedigitalcollection.asme.org
This article presents first-of-a-kind measurements, and complementary computations, of the
flow through the propulsion system of a boundary layer ingesting, twin-engine advanced …

Quality modeling of printed electronics in aerosol jet printing based on microscopic images

H Sun, K Wang, Y Li, C Zhang… - Journal of …, 2017 - asmedigitalcollection.asme.org
Aerosol jet printing (AJP) is a direct write technology that enables fabrication of flexible, fine
scale printed electronics on conformal substrates. AJP does not require the time consuming …

Fundamental machining characteristics of ultrasonic-assisted electrochemical grinding of Ti–6Al–4V

S Li, Y Wu, M Nomura, T Fujii - Journal of …, 2018 - asmedigitalcollection.asme.org
The Ti–6Al–4V is a widely used alloy in the aerospace industry. In order to improve the
grindability of Ti–6Al–4V, a hybrid material removal process is proposed in this study. This …

[HTML][HTML] Fully-turbulent adjoint method for the unsteady shape optimization of multi-row turbomachinery

A Rubino, S Vitale, P Colonna, M Pini - Aerospace Science and …, 2020 - Elsevier
The possibility of taking into account unsteady flow effects if performing turbomachinery
shape optimization is attractive to accurately address inherently time dependent design …

[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 …

Novel method for evaluating intake unsteady flow distortion

M Migliorini, PK Zachos, DG MacManus - Journal of Propulsion and …, 2022 - arc.aiaa.org
Closer integration between the airframe and the propulsion system is expected for future
aircraft to reduce fuel consumption, emissions, weight, and drag. The use of embedded or …