Add to ORKGIt is well known that the aerodynamic study of supersonic jets exhausting from convergent-divergent nozzles is a problem of great importance in many space and aeronautical applications. Various physical phenomena involved in this problem are directly linked to the performance of jet engines. Though off-design operations with either overexpanded o
A time accurate numerical study is presented of an over-expanded Mach 2 circular turbulent jet in wh...
International audienceJets with complex shock-cell structures appear in numerous technological appli...
This paper presents the results of mathematical modeling of the interaction of supersonic twin jet f...
Supersonic air jets from the D'Laval nozzle of designed Mach number 2.0 were experimentally investig...
Experiments and large eddy simulations of a conical convergent divergent nozzle, similar to the nozz...
The present study focuses on the numerical investigation of the Mach 1.86 supersonic jet from the 2-...
International audienceThe transition from regular to Mach reflection in a supersonic planar jet oper...
Shock-induced noise is generated by supersonic jets which are not perfectly expanded. This means tha...
A numerical study of underexpanded axisymmetric supersonic jets is presented. The TVD finitedifferen...
Copyright © 2013 Hiromasa Suzuki et al. This is an open access article distributed under the Creativ...
A two dimensional convergent-divergent nozzle with a rectangular cross section is modelled under amb...
This paper describes a study of sound generated by supersonic jets such as those emanating from the ...
Underexpanded jets have been the subject of many studies for a long time. The most often encountered...
A numerical study, using a mixed finite element/finite volume method on unstructured meshes adapted ...
This paper examines the flow structures emanating from convergent-divergent nozzles with conical sec...
A time accurate numerical study is presented of an over-expanded Mach 2 circular turbulent jet in wh...
International audienceJets with complex shock-cell structures appear in numerous technological appli...
This paper presents the results of mathematical modeling of the interaction of supersonic twin jet f...
Supersonic air jets from the D'Laval nozzle of designed Mach number 2.0 were experimentally investig...
Experiments and large eddy simulations of a conical convergent divergent nozzle, similar to the nozz...
The present study focuses on the numerical investigation of the Mach 1.86 supersonic jet from the 2-...
International audienceThe transition from regular to Mach reflection in a supersonic planar jet oper...
Shock-induced noise is generated by supersonic jets which are not perfectly expanded. This means tha...
A numerical study of underexpanded axisymmetric supersonic jets is presented. The TVD finitedifferen...
Copyright © 2013 Hiromasa Suzuki et al. This is an open access article distributed under the Creativ...
A two dimensional convergent-divergent nozzle with a rectangular cross section is modelled under amb...
This paper describes a study of sound generated by supersonic jets such as those emanating from the ...
Underexpanded jets have been the subject of many studies for a long time. The most often encountered...
A numerical study, using a mixed finite element/finite volume method on unstructured meshes adapted ...
This paper examines the flow structures emanating from convergent-divergent nozzles with conical sec...
A time accurate numerical study is presented of an over-expanded Mach 2 circular turbulent jet in wh...
International audienceJets with complex shock-cell structures appear in numerous technological appli...
This paper presents the results of mathematical modeling of the interaction of supersonic twin jet f...