IIUM Repository

Prof. Dr. Sher Afghan Khan

Profile Picture

Latest Additions

  1. Faheem, Mohammed and Khan, Sher Afghan and Alam, Mohammad Mukhtar and Arputharaj, Beena Stanislaus and Hussain, Fayaz and Al-Mdallal, Qasem M. (2025) Experimental investigation on the flow mixing and core length of a supersonic multiple jet configuration using cross-wire as vortex generators. Aerospace Science and Technology, 162 (110214). pp. 1-17. ISSN 1270-9638 E-ISSN 1626-3219
  2. Mahboobali, Fharukh Ahmed Ghasi and Khan, Ambareen and Akhtar, Mohammad Nishat and Khan, Sher Afghan and Pathan, Khizar Ahmed (2025) Passive control of base flows and impact of quarter rib radius and locations at sonic mach number. Journal of Advanced Research in Numerical Heat Transfer, 30 (1). pp. 47-81. ISSN 2735-0142
  3. Chaudhary, Zakir Ilahi and Khan, Ambareen and Khan, Sher Afghan and Akhtar, Mohammad Nishat and Pathan, Khizar Ahmed (2025) Control of suddenly expanded flow using quarter rib for area ratio 4.84 at Mach 2. Journal of Advanced Research in Experimental Fluid Mechanics and Heat Transfer, 19 (1). pp. 1-29. ISSN 2756-8202
  4. Shaikh, Javed Shoukat and Shetty, Shamitha and Pathan, Khizar Ahmed and Abuj, Narayan Govindrao and Kumar, Krishna and Khan, Sher Afghan and Nema, Anurag A (2025) Numerical modeling and analysis of damping derivatives for a 2D wedge at hypersonic mach numbers and variable pivot points. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 128 (1). pp. 92-107. ISSN 2289-7879
  5. Chaudhary, Zakir Ilahi and Khan, Ambareen and Khan, Sher Afghan and Pathan, Khizar Ahmed (2025) Base pressure control using quarter circle rib in a suddenly expanded duct at screech prone Mach number M = 1.8. CFD Letters, 17 (8). pp. 60-95. ISSN 2180-1363
  6. Bellary, Sayed Ahmed Imran and Khan, Ambareen and Akhtar, Mohammad Nishat and Shahab, Dabir and Khan, Sher Afghan and Pathan, Khizer Ahmed (2025) Numerical simulations of base pressure and its control in a suddenly expanded duct at Mach 1.6 using quarter circular ribs. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 127 (2). pp. 203-233. E-ISSN 2289-7879
  7. Shetty, Shamitha and Mahaboobali, Fharukh Ahmed Ghasi and Khan, Ambareen and Akhtar, Mohammad Nishat and Khan, Sher Afghan and Pathan, Khizar Ahmed (2025) Base pressure control using quarter rib at Mach 1.3: a comprehensive CFD analysis. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 127 (2). pp. 1-32. E-ISSN 2289-7879
  8. Bellary, Sayed Ahmed Imran and Dabir, Shahab Ahmed and Khan, Sher Afghan and Tamhane, Tushar and Shaikh, Javed Habib and Khan, Ambareen (2025) Computational analysis of thrust generated by converging-diverging nozzle at different diverging angles. Journal of Advanced Research in Numerical Heat Transfer, 29 (1). pp. 102-128. ISSN 2735-0142
  9. Shaikh, Javed Shoukat and Kumar, Krishna and Pathan, Khizar Ahmed and Khan, Sher Afghan and Husain, Kharadi Fayaz and Siddiqui, Afreen (2025) Estimation of the damping derivative in pitch for a wedge at supersonic Mach numbers using design of experiments. Journal of Advanced Research in Experimental Fluid Mechanics and Heat Transfer, 18 (1). pp. 106-117. E-ISSN 2756-8202
  10. Khan, Ambareen and Aabid, Abdul and Akhtar, Mohammad Nishat and Khan, Sher Afghan and Baig, Muneer (2025) Supersonic flow control with quarter rib in a duct: An extensive CFD study. International Journal of Thermofluids, 26 (101060). 1- 22. ISSN 2666-2027
  11. Jamadar, Irshad Sikandar and Kumar, Krishna and Jadhav, Pratibha and Bhalerao, Pramod and Khan, Sher Afghan (2025) Prediction of infiltrating ductal carcinoma using Morlet wavelet integrated Kolmogorov Arnold Network. Journal of Advanced Research in Applied Mechanics, 131 (1). pp. 105-118. E-ISSN 2289-7895
  12. Shaikh, Javed Shoukat and Pathan, Khizar Ahmed and Khan, Sher Afghan (2025) Numerical simulation of surface pressure and temperature distribution along a cone at supersonic Mach numbers using CFD. Journal of Advanced Research in Numerical Heat Transfer, 28 (1). pp. 1-26. ISSN 2735-0142
  13. Shetty, Shamitha and Crasta, Asha and Khan, Sher Afghan (2024) Evaluation of derivative in damping in the Newtonian limit for non-planar wedge. Materials Today, 100. pp. 1-3. ISSN 2214-7853
  14. Zuraidi, Nur Husnina Muhamad and Khan, Sher Afghan and Mohammed Sapardi, Mohd Azan and Dixit, Saurav (2024) Passive control of base pressure and the flow development in a duct with sudden expansion at sonic Mach number. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 123 (2). pp. 111-139. E-ISSN 2289-7879
  15. Sambath, Yaknesh , and Natarajan, Rajamurugu and Babu, Prakash K and Raju, K. Ramachandra and Alahmadi, Ahmad Aziz and Alwetaishi, Mamdooh and Khan, Sher Afghan (2024) Comparative analysis of predictive modeling techniques for mechanical properties in dissimilar friction stir welding of AA6061 and AZ31B. Journal of Materials Engineering and Performance, 33 (24). pp. 1-17. ISSN 10599495 E-ISSN 15441024
  16. Ahmad Fakhruddin, Ahmad ‘Afy and Mahboobali, Fharukh Ahmed Ghasi and Khan, Ambareen and Akhtar, Mohammad Nishat and Khan, Sher Afghan and Pathan, Khizar Ahmed (2024) Analysis of base pressure control with ribs at Mach 1.2 using CFD method. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 123 (1). pp. 108-143. ISSN 2289-7879
  17. Kale, Dipak and Arakerimath, Rachayya and Pathan, Khizar Ahmed and Khan, Sher Afghan (2024) Investigation on Water Erosion Behavior of Ti-based Metal Matrix Composite: Experimental Approach. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 122 (2). pp. 71-82. ISSN 2289-7879
  18. Sheikh, Fahim Rahim and Deshmukh, Suresh Pandurang and Ardhapurkar, Purushottam and Pathan, Khizar Ahmed and Shaikh, Sohel Khalil and Khan, Sher Afghan (2024) Modeling and experimental validation of NePCM-Nanofluid-Based PVT system. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 122 (1). pp. 205-222. ISSN 2289-7879
  19. Khan, Ambareen and Aabid, Abdul and Khan, Sher Afghan and Akhtar, Mohammad Nishat and Baig, Muneer (2024) Comprehensive CFD analysis of base pressure control using quarter ribs in sudden expansion duct at sonic Mach numbers. International Journal of Thermofluids, 24. pp. 1-17. ISSN 2666-2027
  20. Shetty, Shamitha and Crasta, Asha and Khan, Sher Afghan and Aabid, Abdul and Baig, Muneer (2024) Effect of sweptback angle of a delta wing on surface pressure distribution at supersonic Mach numbers. Fluid Dynamics and Material Processing, 20 (10). pp. 2353-2376. ISSN 1555-256X E-ISSN 1555-2578

Most Viewed Items

Item titleViews
1Numerical analysis of a microjet-based method for active flow control in convergent-divergent nozzles with a sudden expansion duct1287
2Developments in nanoparticles enhanced biofuels and solar energy in Malaysian perspective: a review of state of the art1190
3A case study of unmanned aerial vehicle (drone) technology and its applications in the COVID-19 pandemic1183
4Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis1176
5Investigation of dual–pass inclined oscillating bed solar dryer for drying of non-parboiled paddy grains1087
6Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.561066
7Numerical investigation of flow field of a non-circular cylinder955
8Optimization and analysis of maximum temperature in a battery pack affected by low to high Prandtl number coolants using response surface methodology and particle swarm optimization algorithm947
9CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows937
10Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow934
11Stability derivatives of a delta wing with straight leading edge in the Newtonian limit928
12Supersonic similitude for oscillating non-planar wedge916
13CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows915
14Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges910
15Exprimental study suddenly expanded flow from correctly expanded nozzles909
16Stabilty derivatives in the newtonian limit899
17Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method893
18Experimental study on the mean flow characteristics of a supersonic multiple jet configuration892
19Position of static cylinder effect on base flows879
20Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions878
21Thermal performance of fined plate mini-channel heat sink877
22Maximum temperature analysis in a Li-ion battery pack cooled by different fluids871
23Effect of angle of incidence on stability derivatives of a wing866
24Counter clockwise rotation of cylinder with variable position to control base flows864
25Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD.852
26Study on tool wear and tool life during milling JFRP using uncoated carbide cutting tool849
27Fluidization dynamics of hydrophobic nanosilica with velocity step changes848
28Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods843
29Challenges and solutions for using liquid fuels in aviation industry842
30Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges840