In this investigation the flow field has been computed by the numerical approach using
Computational Fluid Dynamics (CFD) Analysis to investigate the efficacy of the supersonic …

In this paper, computational fluid dynamic (CFD) analysis and experiments have been
carried out to study the effect of nozzle pressure ratio, ie the ratio of inlet pressure to …

The Aerodynamic base drag because of negative pressure at the backward-facing step is a
general obstacle connected with all the moving projectiles. The aerodynamic base drag is …

This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of
Mach numbers on velocity distribution at different area ratio and nozzle pressure ratio in the …

In the case of flow from the nozzle, the net thrust is the vital and critical consideration. The
net thrust force is the difference of the thrust developed by the jet from the nozzle and the …

In high speed projectiles like rocket, the thrust is created by the convergent divergent nozzle.
The flow from the nozzle is exhausted in the enlarged duct of larger diameter to maximize …

This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect of
area ratio ie the ratio of enlarged duct area to nozzle exit area on velocity distribution along …

This paper deals with finding the optimum fineness ratio, ie ratio of length to maximum
diameter, of human-powered submarine of different shapes to reduce the drag force on the …

This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect
geometry and flow parameters on thrust force created by the flow from convergent-divergent …

A study is undertaken to assess the dynamic control's effectiveness at two supersonic Mach
numbers, 2.2 and 2.58 being considerably large Mach number being very significant in the …