Fan–intake interaction under high incidence

T Cao, NR Vadlamani… - … for Gas Turbines …, 2017 - asmedigitalcollection.asme.org
In this paper, we present an extensive numerical study on the interaction between the
downstream fan and the flow separating over an intake under high incidence. The objectives …

Effects of inlet disturbances on fan stability

KB Lee, M Wilson, M Vahdati - … of Engineering for …, 2019 - asmedigitalcollection.asme.org
This paper investigates the effects of inlet disturbance caused by crosswind on a fan blade
operation and addresses the possible aerodynamic instabilities, which can arise for such a …

[HTML][HTML] A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors

Z Li, D Sun, X Dong, X Sun - Fundamental Research, 2024 - Elsevier
The air intake-compression systems of modern aircraft usually use the aero-engine intake
and fan/compressor as the main components. Inlet-engine compatibility has always been …

Experiment investigation on the effect of inlet circumferential non-uniformity on the stall behaviours in a transonic axial compressor with axisymmetric stall precursor

T Pan, J Yan, Z Yan, D Sun, Q Li - Aerospace Science and Technology, 2022 - Elsevier
The circumferential non-uniformity is becoming a high risk for jet engines in the future with
cutting-edge intake design and undesirable inflow, like crosswind and highly turbulence …

Toward future installations: Mutual interactions of short intakes with modern high bypass fans

NR Vadlamani, T Cao… - Journal of …, 2019 - asmedigitalcollection.asme.org
In this paper, we investigate the coupled interaction between a new short intake design with
a modern fan in a high-bypass ratio civil engine, specifically under the off-design condition …

Simulation of multistage compressor at off-design conditions

F Wang, M Carnevale… - Journal of …, 2018 - asmedigitalcollection.asme.org
Computational fluid dynamics (CFD) has been widely used for compressor design, yet the
prediction of performance and stage matching for multistage, high-speed machines remains …

An energy-based fouling model for gas turbines: EBFOG

N Casari, M Pinelli, A Suman… - Journal of …, 2017 - asmedigitalcollection.asme.org
Fouling is a major problem in gas turbines for aeropropulsion because the formation of
aggregates on the wet surfaces of the machine affects aerodynamic and heat loads. The …

Fan aerodynamics with a short intake at high angle of attack

B Mohankumar, CA Hall… - Journal of …, 2021 - asmedigitalcollection.asme.org
Fans that are designed to maintain thrust at the high angle of attack (AOA) flight condition
could exploit the cruise fuel burn benefit of a shorter intake design. This article considers …

Virtual gas turbine: Pre-processing and numerical simulations

F Wang, M Carnevale, G Lu… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
The design process of a gas turbine engine involves interrelated multi-disciplinary and multi-
fidelity designs of engine components. Traditional component-based design process is not …

Low frequency distortion in civil aero-engine intake

M Carnevale, F Wang… - … of Engineering for …, 2017 - asmedigitalcollection.asme.org
The main role of the intake is to provide a sufficient mass flow to the engine face and a
sufficient flow homogeneity to the fan. Intake-fan interaction off design represents a critical …