Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner
J Duan, X Li, X Li, H Liu - Physics of Fluids, 2021 - pubs.aip.org
A direct numerical simulation of the interaction between a shock wave and the supersonic
turbulent boundary layer in a compression–decompression corner with a fixed 24 deflection …
turbulent boundary layer in a compression–decompression corner with a fixed 24 deflection …
Effects of micro-vortex generators on shock wave structure in a low aspect ratio duct, numerical investigation
The interaction between the shock wave and boundary layer and its induced separation is
an undesirable phenomenon in the design of supersonic systems. The control of this …
an undesirable phenomenon in the design of supersonic systems. The control of this …
Wall temperature effects on shock wave/turbulent boundary layer interaction via direct numerical simulation
Shockwave/turbulent boundary layer interaction on flat plate are investigated by using direct
numerical simulation at different wall temperature of T w/T r= 0.5, 1.0, 2.0 respectively …
numerical simulation at different wall temperature of T w/T r= 0.5, 1.0, 2.0 respectively …
Large eddy simulation of pseudo shock structure in a convergent–long divergent duct
In this paper, the Pseudo shock structure in a convergent–long divergent duct is investigated
using large eddy simulation on the basis of Smagorinsky–Lilly, Wall-Adapting Local Eddy …
using large eddy simulation on the basis of Smagorinsky–Lilly, Wall-Adapting Local Eddy …
Investigation of shock wave control by suction in a supersonic cascade
Z Wang, J Chang, Y Li, C Kong - Aerospace Science and Technology, 2021 - Elsevier
The numerical simulation of suction control on a supersonic cascade is presented in this
paper. The purpose of this study is to enhance the resistance backpressure characteristics of …
paper. The purpose of this study is to enhance the resistance backpressure characteristics of …
Lambda shock behaviors of elliptic supersonic jets; a numerical analysis with modification of RANS turbulence model
SAA Mirjalily - Aerospace Science and Technology, 2021 - Elsevier
Supersonic jets have various applications in different industries, particularly as the
propulsion of air-breathing engines and supersonic ejectors. The present study aimed to …
propulsion of air-breathing engines and supersonic ejectors. The present study aimed to …
Three-dimensional passive and active control methods of shock wave train physics in a duct
In the present work, the physics of a three-dimensional shock train in a convergent-divergent
nozzle is numerically investigated. In this regards, the Ansys-Fluent Software with Algebraic …
nozzle is numerically investigated. In this regards, the Ansys-Fluent Software with Algebraic …
Numerical investigation of over expanded flow behavior in a single expansion ramp nozzle
SM Mousavi, R Pourabidi, E Goshtasbi-Rad - Acta Astronautica, 2018 - Elsevier
The single expansion ramp nozzle is severely over-expanded when the vehicle is at low
speed, which hinders its ability to provide optimal configurations for combined cycle …
speed, which hinders its ability to provide optimal configurations for combined cycle …
Hybrid passive-active control method of a swept shock wave-supersonic wake interaction
In the present study, a hybrid passive-active flow control method is used to investigate the
interaction between a swept shock wave (SSW) generated by a swept compression wall …
interaction between a swept shock wave (SSW) generated by a swept compression wall …
Calibration of the k-ω shear stress transport turbulence model for shock wave boundary layer interaction in a SERN using machine learning
SAA Mirjalily - Engineering Analysis with Boundary Elements, 2023 - Elsevier
Abstract The Single Expansion Ramp Nozzle, which is called SERN, is commonly used in
supersonic and hypersonic aircraft, taking into account the design of integrated …
supersonic and hypersonic aircraft, taking into account the design of integrated …