Computation of unsteady turbomachinery flows: Part 2—LES and hybrids

PG Tucker - Progress in Aerospace Sciences, 2011 - Elsevier
The choice of turbulence model can have a strong impact on results for many
turbomachinery zones. Palliative corrections to them and also transition modeling can have …

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 …

Flow distortion measurements in convoluted aeroengine intakes

PK Zachos, DG MacManus, DG Prieto, N Chiereghin - AiAA Journal, 2016 - arc.aiaa.org
The unsteady flowfields generated by convoluted aeroengine intakes are sources of
instabilities that can compromise the performance of the downstream turbomachinery …

[HTML][HTML] Aerodynamics of a short intake in crosswind

L Boscagli, R Christie, D MacManus… - Aerospace Science and …, 2022 - Elsevier
The next generation of turbofan aero-engines are likely to have an increase in fan diameter
to reduce the specific thrust and increase the overall propulsive efficiency. More compact …

A robust low speed preconditioning formulation for viscous flow computations

Y Colin, H Deniau, JF Boussuge - Computers & Fluids, 2011 - Elsevier
A modification of a low speed preconditioning formulation is proposed to perform robust
computations for both internal and external flows. This formulation is based on the isentropic …

Investigation of jet engine intake distortions caused by crosswind conditions

L Harjes, C Bode, J Grubert, P Frantzheld… - Journal of the Global …, 2020 - journal.gpps.global
ABSTRACT The Propulsion Test Facility of the TU Braunschweig is capable of investigating
future jet engine intakes and fan aerodynamics to a high level of detail. A goal of this facility …

Flow separation control of nacelle in crosswind by microsecond pulsed surface dielectric barrier discharge plasma actuator

Y Jia, H Liang, Q He, Z Su, G Song - Flow, Turbulence and Combustion, 2021 - Springer
Flow separation under crosswind conditions seriously jeopardizes the quality of the
nacelle's flow field. In this paper, microsecond pulsed surface dielectric barrier discharge …

Quasi 3D nacelle design to simulate crosswind flows: Merits and challenges

A Yeung, NR Vadlamani, T Hynes… - International Journal of …, 2019 - mdpi.com
This paper studies the computational modelling of the flow separation over the engine
nacelle lips under the off-design condition of significant crosswind. A numerical framework is …

Separation control for aeroengine intakes, part 1: low-speed investigation of control strategies

CT Wakelam, TP Hynes, HP Hodson… - Journal of Propulsion …, 2012 - arc.aiaa.org
THE modern civil aeroengine intake is expected to provide the fan with a steady, uniformly
distributed flow in a wide variety of operating conditions. This poses a problem to designers …

Multipoint aerodynamic high fidelity shape optimization of an isolated engine nacelle

H Toubin, I Salah El Din, M Meheut - 52nd Aerospace Sciences Meeting, 2014 - arc.aiaa.org
N the current airframe design context, every component is expected to be always better
performing from one generation to the next. In particular, engines are required to reach …