Experimental validation of inviscid linear stability theory applied to an axisymmetric jet
LR Gareev, JS Zayko, AD Chicherina… - Journal of Fluid …, 2022 - cambridge.org
We study the development of perturbations in a submerged air jet with a round cross-section
and a long laminar region (five jet diameters) at a Reynolds number of 5400 by both inviscid …
and a long laminar region (five jet diameters) at a Reynolds number of 5400 by both inviscid …
Reactive experimental control of turbulent jets
DBS Audiffred, AVG Cavalieri, IA Maia… - Journal of Fluid …, 2024 - cambridge.org
We present an experimental study of reactive control of turbulent jets, in which we target
axisymmetric coherent structures, known to play a key role in the generation of sound. We …
axisymmetric coherent structures, known to play a key role in the generation of sound. We …
Active control of jet-plate interaction noise for excited jets by plasma actuators
V Kopiev, G Faranosov, O Bychkov, V Kopiev… - Journal of Sound and …, 2020 - Elsevier
This paper examines the possibility of controlling jet-wing interaction noise by plasma
actuators. The low-frequency part of the jet installation noise is considered as produced by …
actuators. The low-frequency part of the jet installation noise is considered as produced by …
Active control of jet–wing interaction noise using plasma actuators in a narrow frequency band
VF Kopiev, OP Bychkov, VA Kopiev, GA Faranosov… - Acoustical …, 2023 - Springer
For a jet located near the wing, instability waves present in jet mixing layer scatter on the
wing trailing edge, leading to additional noise generation. In this article, the possibility of …
wing trailing edge, leading to additional noise generation. In this article, the possibility of …
Jet installation noise modeling in static and flight conditions using centerline fluctuations
The present work is dedicated to the modeling of the low-frequency part of the jet installation
noise (JIN) in flight conditions. It is known that the properties of JIN can be predicted based …
noise (JIN) in flight conditions. It is known that the properties of JIN can be predicted based …
The modeling of jet-plate interaction noise in the presence of co-flow
G Faranosov, OP Bychkov, V Kopiev… - 25th AIAA/CEAS …, 2019 - arc.aiaa.org
The present work is dedicated to the modelling of the low-frequency part of the jetplate
interaction noise in flight conditions. An analytical model used in the work is based on the …
interaction noise in flight conditions. An analytical model used in the work is based on the …
Transition to turbulence through intermittence in inert and reacting jets
VV Lemanov, VV Lukashov, KA Sharov - Fluid Dynamics, 2020 - Springer
Subsonic flows of different gases in the near field of inert and reacting jets is experimentally
investigated. The jets flowed out of long tubes, 2 to 8 mm in diameter, into an air medium at …
investigated. The jets flowed out of long tubes, 2 to 8 mm in diameter, into an air medium at …
An estimation of the velocity profile for the laminar-turbulent transition in the plane jet on the basis of the theory of stochastic equations and equivalence of measures
AV Dmitrenko, AS Selivanov - Advances in Aerodynamics, 2022 - Springer
The theory of stochastic equations and the theory of equivalence of measures previously
applied to flows in the boundary layer and in the pipe are considered to calculate the …
applied to flows in the boundary layer and in the pipe are considered to calculate the …
Control of instability waves in an unexcited turbulent jet using plasma actuators in a narrow frequency band
VF Kopiev, OP Bychkov, VA Kopiev, GA Faranosov… - Acoustical …, 2021 - Springer
Instability waves developing in the mixing layer of a turbulent jet are in many cases sources
of noise generation (high-speed jets, jets near an aircraft wing, etc.). This study …
of noise generation (high-speed jets, jets near an aircraft wing, etc.). This study …
Plasma-based active closed-loop control of instability waves in unexcited turbulent jet. Part 2. Installed jet.
V Kopiev, G Faranosov, VA Kopiev… - 25th AIAA/CEAS …, 2019 - arc.aiaa.org
The paper considers the possibility of controlling jet-wing interaction noise based on the
results obtained for free jet in the Part I of the study. 1 The main idea is connected with the …
results obtained for free jet in the Part I of the study. 1 The main idea is connected with the …