Dr. S. A. Khan
Dr. S. A. Khan
Professor, Dept. of Mechanical Engineering, IIUM, Kuala Lumpur, Malaysia
Verified email at iium.edu.my - Homepage
Title
Cited by
Cited by
Year
Active control of suddenly expanded flows from overexpanded nozzles
SA Khan, E Rathakrishnan
International Journal of Turbo and Jet Engines 19 (1-2), 119-126, 2002
842002
Control of suddenly expanded flows with micro-jets
SA Khan, E Rathakrishnan
International Journal of Turbo & Jet-Engines 20 (1), 63-81, 2003
822003
Control of suddenly expanded flow
SA Khan, E Rathakrishnan
Aircraft Engineering and Aerospace Technology, 2006
772006
Active control of suddenly expanded flows from underexpanded nozzles
SA Khan, E Rathakrishnan
International Journal of Turbo and Jet Engines 21 (4), 233-254, 2004
772004
Control of suddenly expanded flow from correctly expanded nozzles
SA Khan, E Rathakrishnan
International Journal of Turbo and Jet Engines 21 (4), 255-278, 2004
702004
CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows
SA Khan, A Aabid, MAA Baig
International Journal of Mechanical and Production Engineering Research and …, 2018
382018
Control of base flows with micro jets
MAA Baig, F Al-Mufadi, SA Khan, E Rathakrishnan
International Journal of Turbo & Jet-Engines 28 (1), 59-69, 2011
382011
Control of base pressure with micro‐jets: part I
S Rehman, SA Khan
Aircraft Engineering and Aerospace Technology, 2008
382008
Nozzle expansion level effect on suddenly expanded flow
SA Khan, E Rathakrishnan
International Journal of Turbo and Jet Engines 23 (4), 233, 2006
372006
CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows
KA Pathan, SA Khan, PS Dabeer
2017 2nd International Conference for Convergence in Technology (I2CT), 1104 …, 2017
342017
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
KA Pathan, PS Dabeer, SA Khan
Case studies in thermal engineering 12, 696-700, 2018
332018
osCIILATING SUPERsoNIC DELA WINGs. w CURVED LEADING EDGES
SA Khan, A Crasta
322010
CFD analysis of effect of area ratio on suddenly expanded flows
KA Pathan, SA Khan, PS Dabeer
2017 2nd International Conference for Convergence in Technology (I2CT), 1192 …, 2017
312017
Oscillating Supersonic delta wing with straight Leading Edges
A Crasta, SA Khan
International Journal of Computational Engineering Research 2 (5), 1226-1233, 2012
312012
Active control of suddenly expanded flows from underexpanded nozzles-Part II
SA Khan, E Rathakrishnan
International Journal of Turbo & Jet-Engines 22 (3), 163-184, 2005
312005
Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
SA Khan, A Aabid, FAM Ghasi, AA Al-Robaian, AS Alsagri
CFD Letters 11 (5), 61-71, 2019
282019
Numerical analysis of convergent-divergent nozzle using finite element method
AGM Fharukh, AA Alrobaian, A Aabid, SA Khan
International Journal of Mechanical and Production Engineering Research and …, 2018
282018
CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
KA Pathan, SA Khan, PS Dabeer
2017 2nd International Conference for Convergence in Technology (I2CT), 1121 …, 2017
282017
High Incidence Supersonic similitude for Planar wedge
A Crasta, SA Khan
International Journal of Engineering research and Applications 2 (5), 468-471, 2012
282012
CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
SA Khan, A Aabid, CA Saleel
International Journal of Mechanical and Mechatronics Engineering 1, 2019
262019
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Articles 1–20