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A design of experiment approach as applied to the analysis of diffuser-augmented wind turbines
R Bontempo, R Carandente, M Manna - Energy Conversion and …, 2021 - Elsevier
Since the 1930s ducted-wind-turbines have received considerable attention due to the
possibility of obtaining a significant increase in the extracted power compared to an open …
possibility of obtaining a significant increase in the extracted power compared to an open …
Uncertainty quantification: A stochastic method for heat transfer prediction using LES
In computational fluid dynamics (CFD), it is possible to identify namely two uncertainties:
epistemic, related to the turbulence model, and aleatoric, representing the random-unknown …
epistemic, related to the turbulence model, and aleatoric, representing the random-unknown …
Low frequency distortion in civil aero-engine intake
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 …
sufficient flow homogeneity to the fan. Intake-fan interaction off design represents a critical …
Analysis and evaluation of the momentum theory errors as applied to propellers
R Bontempo, M Manna - AIAA Journal, 2016 - arc.aiaa.org
This paper offers an analytical formulation of the two errors embodied in the momentum
theory. The first one originates from the use of the differential form of the axial momentum …
theory. The first one originates from the use of the differential form of the axial momentum …
Lip stall suppression in powered intakes
This work describes a computational study into lip stall in subsonic civil aircraft intakes and
its alleviation by action of the fan. Beyond a certain flow incidence, the lower lip of a civil …
its alleviation by action of the fan. Beyond a certain flow incidence, the lower lip of a civil …
Steady turbulent flow computations using a low mach fully compressible scheme
A Garcia-Uceda Juarez, A Raimo, E Shapiro… - AIAA Journal, 2014 - arc.aiaa.org
A recently proposed modification to fully compressible schemes significantly improves the
resolution of low-Mach-number features, tackling the problem of excessive numerical …
resolution of low-Mach-number features, tackling the problem of excessive numerical …
[HTML][HTML] Verification of the axial momentum theory for propellers with a uniform load distribution
R Bontempo, M Manna - International Journal of Turbomachinery …, 2019 - mdpi.com
The paper provides an evaluation of the errors embodied in the Axial Momentum Theory
(AMT) as applied to a uniformly loaded actuator disk model without wake rotation. Although …
(AMT) as applied to a uniformly loaded actuator disk model without wake rotation. Although …
[PDF][PDF] Numerical studies into intake flow for fan forcing assessment
Recent trends in design for civil intakes lead towards shorter diffuser sections, unorthodox
installations and more loaded lips. All these features increase the risk of lip stall in flight at …
installations and more loaded lips. All these features increase the risk of lip stall in flight at …
Pulsating coolant ejection effects downstream of supersonic trailing edge
Trailing edge blowing is used in a great variety of applications. In particular, high-pressure
turbines bleed about 3% of the engine core massflow through a rear slot of the inlet guide …
turbines bleed about 3% of the engine core massflow through a rear slot of the inlet guide …
Low frequency distortion in civil aero-engine intake
The main role of the intake is to provide a sufficient mass flow to the engine face and
sufficient flow homogeneity to the fan. Intake-fan interaction off design represents a critical …
sufficient flow homogeneity to the fan. Intake-fan interaction off design represents a critical …