This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of area ratio i.e. the ratio of enlarged duct area to nozzle exit area on velocity distribution along axis by varying the nozzle pressure ratios. The convergent-divergent nozzle and suddenly expanded circular duct of larger cross-sectional area are used for analysis. The analysis is done for Mach number 2.0 by varying the area ratios and nozzle pressure ratios. The area ratios for the analysis are 1, 2, 4, 6, 8, 10 and 12. The values of nozzle pressure ratios considered are 2, 4, 6, 8, 10 and 12. The results are compared with the help of graphs and tables. By observing all the results it can be concluded that the flow field in the enlarged duct is strong...
Abstract- The experiments are carried out to study the effect of different levels of over expansion ...
The drag force is an essential factor in any projectile from road vehicles to rocket or aircraft. Th...
Micro jets are used in the present experimental study as an active control. Flow from converging noz...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of Mach numbe...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and ...
In this investigation the flow field has been computed by the numerical approach using Computational...
The experiments were carried out to assess the effect of Mach number on base pressure and control ef...
The contribution from the base drag due to the sub-atmospheric pressure is significant. It can be mo...
As the need for missiles and rockets has increased exponentially, the challenges associated with the...
Airflow from convergent axisymmetric nozzle expanded suddenly into circular duct of larger cross-sec...
In the case of flow from the nozzle, the net thrust is the vital and critical consideration. The net...
Researches over the recent past in the field of aerodynamic vehicles have been concerned with the p...
Abstract — In this paper results of experimental studies conducted to study the development of flow ...
In this paper results of experimental studies conducted to study the development of flow from a conv...
Airflow from convergent-divergent axisymmetric nozzles expanded into circular duct of higher area we...
Abstract- The experiments are carried out to study the effect of different levels of over expansion ...
The drag force is an essential factor in any projectile from road vehicles to rocket or aircraft. Th...
Micro jets are used in the present experimental study as an active control. Flow from converging noz...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of Mach numbe...
This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and ...
In this investigation the flow field has been computed by the numerical approach using Computational...
The experiments were carried out to assess the effect of Mach number on base pressure and control ef...
The contribution from the base drag due to the sub-atmospheric pressure is significant. It can be mo...
As the need for missiles and rockets has increased exponentially, the challenges associated with the...
Airflow from convergent axisymmetric nozzle expanded suddenly into circular duct of larger cross-sec...
In the case of flow from the nozzle, the net thrust is the vital and critical consideration. The net...
Researches over the recent past in the field of aerodynamic vehicles have been concerned with the p...
Abstract — In this paper results of experimental studies conducted to study the development of flow ...
In this paper results of experimental studies conducted to study the development of flow from a conv...
Airflow from convergent-divergent axisymmetric nozzles expanded into circular duct of higher area we...
Abstract- The experiments are carried out to study the effect of different levels of over expansion ...
The drag force is an essential factor in any projectile from road vehicles to rocket or aircraft. Th...
Micro jets are used in the present experimental study as an active control. Flow from converging noz...