A review of the shock-dominated flow in a hypersonic inlet/isolator
H Huang, H Tan, F Li, X Tang, Y Qin, LB **ement cooling with the use of synthetic jet
P Gil, J Wilk - International Journal of Thermal Sciences, 2020 - Elsevier
The paper presents experimental studies on heat transfer phenomena which occurs during
the im**ement cooling with the use of synthetic jet. The synthetic jet was created by a …
the im**ement cooling with the use of synthetic jet. The synthetic jet was created by a …
Plasma synthetic jet actuators for active flow control
The plasma synthetic jet actuator (PSJA), also named as sparkjet actuator, is a special type
of zero-net mass flux actuator, driven thermodynamically by pulsed arc/spark discharge …
of zero-net mass flux actuator, driven thermodynamically by pulsed arc/spark discharge …
Model-free short-term fluid dynamics estimator with a deep 3D-convolutional neural network
Deep learning models are not yet fully applied to fluid dynamics predictions, while they are
the state-of-the-art solution in many other areas ie video and language processing, finance …
the state-of-the-art solution in many other areas ie video and language processing, finance …
Study on inner characteristics of plasma synthetic jet actuator and geometric effects
W Zhang, X Geng, Z Shi, S ** - Aerospace Science and Technology, 2020 - Elsevier
In order to further study the inner characteristics of the plasma synthetic jet actuator (PSJA)
which consists of a cavity, two electrodes and a lid with orifice, a two-dimensional numerical …
which consists of a cavity, two electrodes and a lid with orifice, a two-dimensional numerical …
Characterization of plasma synthetic jet actuator with Laval-shaped exit and application to drag reduction in supersonic flow
W **e, Z Luo, L Hou, Y Zhou, Q Liu, W Peng - Physics of Fluids, 2021 - pubs.aip.org
ABSTRACT A plasma synthetic jet (PSJ) actuator (PSJA) with a Laval-shaped exit is
investigated using a numerical method alongside a PSJA with a straight-shaped exit for …
investigated using a numerical method alongside a PSJA with a straight-shaped exit for …
Airfoil flow separation control with plasma synthetic jets at moderate Reynolds number
An array of 26 plasma synthetic jet actuators (PSJA) is flush-mounted on a NACA-0015
airfoil model to control the leading-edge flow separation at moderate Reynolds number …
airfoil model to control the leading-edge flow separation at moderate Reynolds number …