Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76884/1/AIAA-1992-321-143.pd
Experimental investigations were carried out in 0.3m trisonic wind tunnel at NAL to study the effect...
This Philosophiae Doctor thesis presents the motivation, objectives and reasoning behind the undert...
A combined analytical and numerical study is conducted to investigate the asymmetric cap-shock non-u...
178-188<span style="font-size:11.0pt;line-height:115%; font-family:" calibri","sans-serif";mso-asci...
Underexpanded axisymmetric jets are studied numerically using a full Navier-Stokes solver. Emphasis ...
A numerical study of underexpanded axisymmetric supersonic jets is presented. The TVD finitedifferen...
This work aims at developing/combining numerical tools adapted to the simulation of the near field o...
This paper numerically investigates the effect of flow non-ideality on the Mach disk pattern occurri...
An approximate analytical model has been developed for computing the first cycle of the shock struct...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76634/1/AIAA-1989-80-667.pd
A two dimensional, nonaxisymmetric Euler solution in a geometry representative of a jet engine confi...
A Neumann solution for inviscid external flow was coupled to a modified Reshotko-Tucker integral bou...
The aim of this work is the study of the fluid dynamic structure of underexpanded hydrogen jets by ...
An iterative method for blade design based on Euler solver and described in an earlier paper is used...
Weakly and strongly underexpanded, axisymmetric, supersonic jets are studied using unstructured, tri...
Experimental investigations were carried out in 0.3m trisonic wind tunnel at NAL to study the effect...
This Philosophiae Doctor thesis presents the motivation, objectives and reasoning behind the undert...
A combined analytical and numerical study is conducted to investigate the asymmetric cap-shock non-u...
178-188<span style="font-size:11.0pt;line-height:115%; font-family:" calibri","sans-serif";mso-asci...
Underexpanded axisymmetric jets are studied numerically using a full Navier-Stokes solver. Emphasis ...
A numerical study of underexpanded axisymmetric supersonic jets is presented. The TVD finitedifferen...
This work aims at developing/combining numerical tools adapted to the simulation of the near field o...
This paper numerically investigates the effect of flow non-ideality on the Mach disk pattern occurri...
An approximate analytical model has been developed for computing the first cycle of the shock struct...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76634/1/AIAA-1989-80-667.pd
A two dimensional, nonaxisymmetric Euler solution in a geometry representative of a jet engine confi...
A Neumann solution for inviscid external flow was coupled to a modified Reshotko-Tucker integral bou...
The aim of this work is the study of the fluid dynamic structure of underexpanded hydrogen jets by ...
An iterative method for blade design based on Euler solver and described in an earlier paper is used...
Weakly and strongly underexpanded, axisymmetric, supersonic jets are studied using unstructured, tri...
Experimental investigations were carried out in 0.3m trisonic wind tunnel at NAL to study the effect...
This Philosophiae Doctor thesis presents the motivation, objectives and reasoning behind the undert...
A combined analytical and numerical study is conducted to investigate the asymmetric cap-shock non-u...
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