In high-speed fluid dynamics, base pressure controls find many engineering applications,
such as in the automobile and defense industries. Several studies have been reported on …

The experimental analysis of base pressure in a high-speed compressible flow is carried
out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen …

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 …

In many applications like the aircraft or the rockets/missiles, the flow from a nozzle needs to
be expanded suddenly in an enlarged duct of larger diameter. The enlarged duct is provided …

This paper aims to numerically simulate the flow field for wedge, cone, and ogives. Usually,
wedge shapes are used as a stabilizing surface for supersonic projectiles like rockets …

This paper aims to estimate the surface pressure of a wedge at hypersonic Mach numbers at
a considerable angle of incidence. The Ghosh similitude, corresponding strip theory, and …

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 …

Submersible vessels designed to operate at low speeds are often designed with an intricate
exostructure, as well as other elements that are located outside of the main pressure hull …