Flow characteristics of coaxial-nozzle ejector for PEMFC hydrogen recirculation system
M Yu, C Wang, L Wang, X Wang - Applied Thermal Engineering, 2024 - Elsevier
Multi-nozzle ejectors are an effective method to overcome the conflicts between the ejector
fixed geometry and various system operating conditions in the ejector-driven proton …
fixed geometry and various system operating conditions in the ejector-driven proton …
Experimental analysis of an under-expanded jet interacting with a tangential flat plate: Flow visualizations and wall pressure statistics
A statistical characterization of the pressure load induced on a rigid surface by a high speed
compressible jet is carried out experimentally on a simple configuration consisting of a …
compressible jet is carried out experimentally on a simple configuration consisting of a …
Large Eddy Simulation of a supersonic air ejector
This paper presents a study on the flow topology in the mixing chamber of a supersonic
ejector using Large Eddy Simulation (LES). To this end, a supersonic air ejector of squared …
ejector using Large Eddy Simulation (LES). To this end, a supersonic air ejector of squared …
Modal analysis of the laminar boundary layer instability and tonal noise of an airfoil at Reynolds number 150,000
A direct numerical simulation of the flow field around a controlled-diffusion airfoil within an
anechoic wind-tunnel at 5° incidence and a high Reynolds number of 1.5× 10 5 is performed …
anechoic wind-tunnel at 5° incidence and a high Reynolds number of 1.5× 10 5 is performed …
Spatiotemporal superresolution measurement based on POD and sparse regression applied to a supersonic jet measured by PIV and near-field microphone
The present study proposed the framework of the spatiotemporal superresolution
measurement based on the sparse regression with dimensionality reduction using the …
measurement based on the sparse regression with dimensionality reduction using the …
Overview of the use of large-eddy simulations in jet aeroacoustics
AS Lyrintzis, M Coderoni - AIAA Journal, 2020 - arc.aiaa.org
The current state of the use of large-eddy simulations (LESs) in jet aeroacoustics is
reviewed. Various computational techniques are discussed, as well as methods to extend …
reviewed. Various computational techniques are discussed, as well as methods to extend …
On the influence of uncertainty in computational simulations of a high-speed jet flow from an aircraft exhaust
A classic approach to Computational Fluid Dynamics (CFD) is to perform simulations with a
fixed set of variables in order to account for parameters and boundary conditions. However …
fixed set of variables in order to account for parameters and boundary conditions. However …
On the influence of the nozzle exhaust initial conditions on the near field acoustic pressure
In this paper, the acoustic pressure generated in the near field of a single stream cold jet is
investigated. The analysis is focused on the effect of the initial conditions at the nozzle exit …
investigated. The analysis is focused on the effect of the initial conditions at the nozzle exit …
Broadband shock-associated noise modelling for high-area-ratio under-expanded jets
V Gryazev, A Kalyan, AP Markesteijn… - The Journal of the …, 2021 - pubs.aip.org
Broadband shock-associated noise (BBSAN) is an important component of supersonic jet
noise for jets at off-design conditions when the pressure at the nozzle exit is different from …
noise for jets at off-design conditions when the pressure at the nozzle exit is different from …
Some insights into the screech tone of under-expanded supersonic jets using dynamic mode decomposition
Jet screech is an intense pure tone which has attracted decades of research interest due to
its possible detrimental effect on engineering structures. Its modes and closure mechanisms …
its possible detrimental effect on engineering structures. Its modes and closure mechanisms …