IIUM Repository

Prof. Dr. Sher Afghan Khan

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Latest Additions

  1. 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
  2. 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
  3. 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
  4. 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.
  5. 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
  6. Aabid, Abdul and Khan, Sher Afghan (2020) Determination of wall pressure flows at supersonic Mach numbers. Materials Today. pp. 1-6. ISSN 2214-7853
  7. 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
  8. 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
  9. 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
  10. 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
  11. 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
  12. SHAMITHA, A and Crasta, Asha and Khan, Sher Afghan and VASAVI, P (2020) Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 10 (special Issue). pp. 208-218. ISSN 2249–6890 E-ISSN 2249–8001
  13. Pathan, Khizar Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2020) An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows. Journal of Thermal Engineering,, 6 (2 (Special Issue 11)). pp. 15-23. E-ISSN 2148-7847
  14. Siddiqui, Umair and Ansari, Emad and Khan, Sher Afghan and Patil, Rajesh (2020) Numerical investigation of secondary peaks in Nusselt profile under water jet impingement. Journal of Thermophysics and Heat Transfer, 34 (2 (April-June)). pp. 421-428. ISSN 0887-8722 E-ISSN 1533-6808
  15. Pathan, Khizer Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2020) Enlarge duct length optimization for suddenly expanded flows. Advances in Aircraft and Spacecraft Science, 7 (3). pp. 203-214. ISSN 2287-528X E-ISSN 2287-5271
  16. Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2020) Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number. Test Engineering & Management, 83 (2). pp. 13808-13819. ISSN 0193-4120
  17. Khan, Sher Afghan and Bashir, Musavir and Baig, Maugal Ahmed Ali and Mehaboob Ali, Fharukh Ahmed Ghasi (2020) Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics. CFD Letters, 12 (3). pp. 1-10. ISSN 2180-1363
  18. Mohd Sajali, Muhammad Fahmi and Aabid, Abdul and Khan, Sher Afghan and Mehaboobali, Fharukh Ahmed Ghasi and Sulaeman, Erwin (2019) Numerical investigation of flow field of a non-circular cylinder. CFD Letters, 11 (5). pp. 37-49. ISSN 2180-1363
  19. Mohd Zakuan, Muhammad Amir Mirza and Aabid, Abdul and Khan, Sher Afghan (2019) Modelling and structural analysis of three-dimensional wing. International Journal of Engineering and Advanced Technology, 9 (1). pp. 6820-6828. ISSN 2249-8958
  20. Aabid, Abdul and Chaudhary, Zakir Ilahi and Khan, Sher Afghan (2019) Modelling and analysis of convergent divergent nozzle with sudden expansion duct using finite element method. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 63 (1). pp. 34-51. ISSN 2289-7879

Most Viewed Items

Item titleViews
1Active control of flow through the nozzles at sonic Mach number1021
2Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field1015
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges985
4Influence of micro jets on wall pressure for area ratio 3.24956
5The effect of micro jets on wall pressure for sonic under expanded flow937
6Studies on wall pressure flow control by micro jets for high area ratio929
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios926
8Control of suddenly expanded flow at low supersonic Mach numbers884
9Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56855
10Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge843
11Effect of level of expansion and inertia level in a suddenly expanded flow824
12Control of base pressure with micro jets for area ratio 2.4824
13Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 815
14Stabilty derivatives in the newtonian limit815
15Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 808
16Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow807
17An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle806
18Stability derivatives of a delta wing with straight leading edge in the Newtonian limit805
19Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges799
20Supersonic similitude for oscillating non-planar wedge792
21Effect of mach number on wall pressure flow field for area ratio 2.56791
22Control of base pressure with micro jets:part-I790
23Base pressure studies from over expanded nozzle for area ratio 2.56789
24Effect of mach number in a suddenly expanded flow for area ratio 4.84788
25Experimental study of suddenly expanded flow from correctly expanded nozzles783
26Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow773
27Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD772
28Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 768
29Active control of base pressure in suddenly expanded flow for area ratio 4.84759
30Effectiveness of micro-jets at different level of expansion759