IIUM Repository

Prof. Dr. Sher Afghan Khan

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  1. Aabid, Abdul and Khan, Sher Afghan (2020) Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods. Arabian Journal of Science and Engineering. pp. 1-30. ISSN 2193-567X E-ISSN 2191-4281 (In Press)
  2. Al-Khalifah, Turki and Aabid, Abdul and Khan, Sher Afghan (2020) Regression analysis of flow parameters at high Mach numbers. Solid State Technology, 63 (6). pp. 5473-5488. ISSN 0038-111X
  3. Afzal, Asif and Aabid, Abdul and Khan, Ambareen and Khan, Sher Afghan and Rajak, Upendra and Verma, Tikendra Nath and Kumar, Rahul (2020) Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded high-speed aerodynamic flows. Aerospace Science and Technology, 107. pp. 1-30. ISSN 1270-9638
  4. Dabhade, Ameya and Pathan, Khizar Ahmed and Khan, Sher Afghan and Jadhav, Akash (2020) Design and development of chassis for formula student vehicle. International Journal of Advanced Research in Engineering and Technology (IJARET), 11 (10). pp. 1121-1130. ISSN 0976-6480 E-ISSN 0976-6499
  5. Quadros, Jaimon Dennis and Khan, Sher Afghan and T., Prashanth (2020) Experimental and numerical investigation of expansion corner effects on isolator performance. International Journal of Turbo & Jet Engines, Ahead of print. pp. 1-8. ISSN 0334-0082 E-ISSN 2191-0332 (In Press)
  6. Quadros, Jaimon D. and Khan, Sher Afghan and Sapkota, Sanjeev and John, Vikrama and Prashanth, T (2020) On recirculation region length of suddenly expanded supersonic flows, using CFD and fuzzy logic. International Journal of Computational Fluid Dynamics. pp. 1-17. ISSN 1061-8562 E-ISSN 1029-0257 (In Press)
  7. Shaikh, Sohel Khalil and Pathan, Khizar Ahmed and Chaudhary, Zakir Ilahi and Khan, Sher Afghan (2020) CFD analysis of an automobile catalytic converter to obtain flow uniformity and to minimize pressure drop across the monolith. CFD Letters, 12 (9). pp. 116-128. ISSN 2180-1363
  8. Shaikh, Sohel Khalil and Pathan, Khizer Ahmed and Chaudhary, Zakir Ilahi and Marlpalle, B. G. and Khan, Sher Afghan (2020) An investigation of three-way catalytic converter for various inlet cone angles using CFD. CFD Letters, 12 (9). pp. 76-90. ISSN 2180-1363
  9. Afzal, Asif and Khan, Sher Afghan and Islam, Md. Tariqul and Jilte, R. D. and Khan, Ambareen and Soudagar, Manzoore Elahi M (2020) Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers. Physics of Fluids, 32 (9). pp. 1-18. ISSN 1070-6631 E-ISSN 1089-7666
  10. Mokashi, Imran and Khan, Sher Afghan and Abdullah, Nur Azam and Azami, Muhammad Hanafi and Afzal, Asif (2020) Maximum temperature analysis in a Li-ion battery pack cooled by different fluids. Journal of Thermal Analysis and Calorimetry, 141. pp. 2555-2571. ISSN 1388-6150 E-ISSN 1588-2926
  11. Mohd, Umair Siddique and Ansari, Emaad and Khan, Sher Afghan and Gulhane, Nitin Parashram and Patil, Rajesh (2019) Numerical investigation of nondimensional constant and empirical relation representing nusselt profile nonuniformity. Journal of Thermophysics and Heat Transfer, 34 (1). pp. 215-229. ISSN 0887-8722 E-ISSN 1533-6808
  12. Quadros, Jaimon Dennis and Khan, Sher Afghan and Prashanth, T. (2020) Experimental and numerical investigation of suddenly expanded flow field for supersonic Mach numbers with and without annular cavities. International Journal of Fluid Mechanics Research, 47 (4). pp. 337-356. ISSN 2152-5102 E-ISSN 2152-5110
  13. Asadullah, Mohammed and Khan, Sher Afghan and Asrar, Waqar and Sulaeman, Erwin (2020) Position of static cylinder effect on base flows. In: 1st International Conference on Data Science, Machine Learning and Applications, 2019, 29th - 30th March 2019, Hyderabad, India.
  14. Quadros, Jaimon Dennis and Khan, Sher Afghan (2020) Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD. Journal of Applied Fluid Mechanics, 13 (2). pp. 499-511. ISSN 1735-3572 E-ISSN 1735-3645
  15. Aabid, Abdul and Khan, Sher Afghan (2020) Determination of wall pressure flows at supersonic Mach numbers. Materials Today. pp. 1-6. ISSN 2214-7853
  16. Kumar, Rahul and Kumar, Veera Sesha and Butt, M. Mursaleen and Sheikh, Nazir Ahmed and Khan, Sher Afghan and Afzal, Asif (2020) Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions. Applied Thermal Engineering, 179. pp. 1-32. ISSN 1359-4311
  17. Siddiqui, Mohammad Umair and Ansari, Emad and Khan, Sher Afghan and Patil, Rajesh (2020) Numerical investigation of semi-empirical relation representing nusselt number under waterjet impingement. Journal of Thermophysics and Heat Transfer, 34 (3). pp. 579-590. ISSN 0887-8722
  18. Ansari, Emad and Siddiqui, M. Umair and Khan, Sher Afghan and Akhtar, Mohammad Nishat and Ilmi, Abu Bakar (2020) Numerical investigation of mathematical non-dimensional constant representing smoothness in the Nusselt profile. CFD Letters, 12 (6). pp. 16-27. ISSN 2180-1363
  19. Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2020) Estımatıon of hypersonıc unsteady and qausı-steady dampıng derıvatıves for a delta wings at large incıdence. International Journal of Advanced Science and Technology, 29 (6). pp. 6844-6863. ISSN 2005-4238 E-ISSN 2207-6360
  20. Afifi, Azmil and Aabid, Abdul and Khan, Sher Afghan (2020) Numerical investigation of splitter plate effect on the bluff body using finite volume method. Materials Today: Proceedings (10.1016/j.matpr.2020.05.559). pp. 1-10. ISSN 2214-7853

Most Viewed Items

Item titleViews
1Active control of flow through the nozzles at sonic Mach number1062
2Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field1060
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges1026
4Influence of micro jets on wall pressure for area ratio 3.24995
5The effect of micro jets on wall pressure for sonic under expanded flow986
6Studies on wall pressure flow control by micro jets for high area ratio981
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios972
8Control of suddenly expanded flow at low supersonic Mach numbers927
9Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56905
10Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge888
11Control of base pressure with micro jets for area ratio 2.4878
12Effect of level of expansion and inertia level in a suddenly expanded flow866
13An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle857
14Stabilty derivatives in the newtonian limit856
15Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 856
16Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 854
17Stability derivatives of a delta wing with straight leading edge in the Newtonian limit853
18Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges844
19Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow842
20Base pressure studies from over expanded nozzle for area ratio 2.56835
21Effect of mach number on wall pressure flow field for area ratio 2.56833
22Control of base pressure with micro jets:part-I831
23Supersonic similitude for oscillating non-planar wedge828
24Experimental study of suddenly expanded flow from correctly expanded nozzles827
25Effect of mach number in a suddenly expanded flow for area ratio 4.84824
26Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD817
27Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 813
28Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow812
29Active control of base pressure in suddenly expanded flow for area ratio 4.84801
30Effectiveness of micro-jets at different level of expansion797