[HTML][HTML] A critical review of supersonic flow control for high-speed applications

A Aabid, SA Khan, M Baig - Applied Sciences, 2021‏ - mdpi.com
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 …

Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods

A Aabid, SA Khan - Arabian Journal for Science and Engineering, 2021‏ - Springer
In high-speed fluid dynamics, the control of base pressure finds many engineering
applications such as automobile industry and defense applications. Several studies have …

CFD analysis of compressible flows in a convergent-divergent nozzle

SA Khan, OM Ibrahim, A Aabid - Materials Today: Proceedings, 2021‏ - Elsevier
A Nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase
the outflow velocity and control fluid flow direction. To obtain the nozzle duct's shock pattern …

Influence of expansion level on base pressure and reattachment length

KA Pathan, PS Dabeer, SA Khan - CFD Letters, 2019‏ - akademiabaru.com
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 …

Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method

SA Khan, A Aabid, FAM Ghasi, AA Al-Robaian… - CFD Letters, 2019‏ - akademiabaru.com
Whereas the demand for missiles and rockets has exponentially augmented, but the
difficulties related to the gas dynamics of these vehicles remains to be a threat. Whenever …

[PDF][PDF] Inspection of supersonic flows in a CD nozzle using experimental method

MH Azami, M Faheem, A Aabid, I Mokashi… - International Journal of …, 2019‏ - academia.edu
In high speed flows nozzles are used to change pressure energy to kinetic energy which in
turn is used to produce thrust. In a converging-diverging nozzle, flow is augmented from …

Analysis of parameters affecting thrust and base pressure in suddenly expanded flow from nozzle

KA Pathan, S Ashfaq, PS Dabeer, SA Khan - 2019‏ - lrc.acharyainstitutes.in
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 …

Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics

SA Khan, M Bashir, MAA Baig, FAGM Ali - CFD Letters, 2020‏ - akademiabaru.com
The analysis of aerodynamic forces on two-dimensional airfoils and flow phenomena
associated with different Reynolds number has been widely investigated for aerospace …

[PDF][PDF] Experimental research on wall pressure distribution in CD nozzle at mach number 1.1 for area ratio 3.24

SA Khan, I Mokashi, A Aabid… - International Journal of …, 2019‏ - researchgate.net
In this experimental investigation the work reported is about the influence of control on the
flow field in the suddenly expanded duct at low supersonic Mach number. A Convergent …

Optimization of two-dimensional wedge flow field at supersonic Mach number

SA Khan, A Aabid, I Mokashi, AA Al-Robaian… - CFD Letters, 2019‏ - akademiabaru.com
In the present condition, there is a high demand for exact solutions through analytical,
computational and measurements in the field of aerospace engineering. For wind tunnel …