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K. Matsuo, Y. Miyazato, H. Kim (1999)
Shock train and pseudo-shock phenomena in internal gas flowsProgress in Aerospace Sciences, 35
(2008)
Starukhin, The Processes of Deceleration of Supersonic Flows in Ducts
Y. Gounko, I. Mazhul’ (2018)
Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inletThermophysics and Aeromechanics, 25
I. Mazhul’, Y. Gounko (2018)
Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inletThermophysics and Aeromechanics, 25
L. Sun, H. Sugiyama, Kazuhide Mizobata, Koichi Fukuda (2003)
Numerical and experimental investigations on the mach 2 pseudo-shock wave in a square ductJournal of Visualization, 6
(2018)
Visualization of Physical and Mathematical Modeling Data in Gas Dynamics
(2014)
Methods of visualization of vortex flows in computational gas dynamics and their application in solving applied problems, Scientific and Technical Information Technologies, Mechanics and Optics
DANIEL Reda, JOHN Murphy (1972)
Shock wave-turbulent boundary layer interactions in rectangular channels.AIAA Journal, 11
(1985)
Flow structure and maximum static pressures at the entry and throat of plane air inlets at high supersonic velocities
(1988)
Pseudo-shock and separation flow in ducts of rectangular cross section
D. Reda, J. Murphy (1973)
Shock wave-turbulent boundary layer interactions in rectangular channels. II - The influence of sidewall boundary layers on incipient separation and scale of the interaction.
A. Zheltovodov, D. Knight (2011)
Shock Wave–Boundary-Layer Interactions: Ideal-Gas Shock Wave???Turbulent Boundary-Layer Interactions (STBLIs) in Supersonic Flows and Their Modeling: Two-Dimensional Interactions
A. Lokotko, A. Kharitonov (2006)
On the possible formation of a vortex flow in a supersonic inlet with three-dimensional compressionFluid Dynamics, 41
(1974)
Experimental investigation of supersonic turbulent boundary layer separation in a cylindrical duct
V. Kornilov (2017)
Three-dimensional turbulent near-wall flows in streamwise corners: Current state and questionsProgress in Aerospace Sciences, 94
(2017)
Influence of back pressure on the flow in the diffuser of a supersonic air inlet
(2009)
Experimental Investigation of Separated Flows in Ducts
(1990)
The influence of entrance conditions of a rectangular channel on the structure of the internal supersonic flow
C.‐P. Wang, Xuang Tian, Keming Cheng, Y-Z Wu (2008)
Numerical analysis of pseudo-shock flow diffusion phenomenon in variable cross-section ductsProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 222
D. Reda, J. Murphy (1973)
Sidewall Boundary-Layer Influence on Shock Wave/Turbulent Boundary-Layer InteractionsAIAA Journal, 11
F. Gnani, H. Zare-Behtash, K. Kontis (2016)
Pseudo-shock waves and their interactions in high-speed intakesProgress in Aerospace Sciences, 82
Robert Leiken (2011)
A User’s Guide
Ignatiy Mazhul, Youry Gounko (2019)
COMPARISON OF PSEUDO-SHOCK FLOWS IN DIVERGENT DIFFUSERS OF AXISYMMETRIC AND TWO-DIMENSIONAL INLETS OF INTERNAL COMPRESSIONPerm National Research Polytechnic University Aerospace Engineering Bulletin
(2016)
and K
Results of a numerical study of the flow structure in the rectangular duct of a model air inlet with the interaction of the shock wave generated by the inlet cowl with the turbulent boundary layer on the inner duct surfaces are reported. A configuration involving a convergent entrance section and a constant-cross-section throat was analyzed. The numerical simulation of the three-dimensional flow with free-stream Mach number M = 4 was performed on the basis of the Reynolds-averaged Navier-Stokes equations and the k-ω SST model of turbulence. As a result of the calculations, the limit streamlines and the distributions of static pressure on the duct surfaces, as well as the distributions of total pressure and the fields of Mach number in duct cross sections were obtained. The structure of the flow is analyzed and the possibility of occurrence of longitudinal vortex structures in the corner region of the intake-duct throat is shown.
Thermophysics and Aeromechanics – Springer Journals
Published: Dec 23, 2020
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