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Prof. Dr. Sher Afghan Khan

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  1. 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
  2. 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
  3. 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
  4. 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
  5. 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
  6. 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
  7. 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
  8. 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
  9. 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
  10. 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
  11. 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
  12. 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
  13. Delvi, Hamza Afser and Faheem, Mohammed and Aabid, Abdul and Math, M.C. and Khan, Sher Afghan (2020) Investigation of characteristics of spark ignition engine fuelled with ethanol-gasoline blends using Iso-octane additive. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66 (1). pp. 151-163. ISSN 2289-7879
  14. Sethuraman, Vigneshvaran and Rajendaran, Parvathy and Khan, Sher Afghan (2020) Base and wall pressure control using cavities and ribs in suddenly expanded flows -an overview. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66 (1). pp. 120-134. ISSN 2289-7879
  15. Bashir, Musavir and Khan, Sher Afghan and Choudhary, Zakir Ilahi and Shinde, V. S. (2020) Wall Pressure Measurements Beneath the Supersonic Jets in an Abruptly Augmented Nozzle. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 66 (2). pp. 20-31. ISSN 2289-7879
  16. Aabid, Abdul and Jyothi, J and Zayan, Jalal Mohammed and Khan, Sher Afghan (2019) Experimental and numerical investigation on gas turbine blade with the application of thermal barrier coatings. Advances in Materials Research, 8 (4). pp. 275-293. ISSN 2234-0912 E-ISSN 2234-179X
  17. Prashant, Jagadesh and Antony, Alappat Joseph and Khan, Sher Afghan (2020) Experimental investigation on the performance of single spark ignition and twin spark ignition engine fuelled with ethanol-gasoline blends. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 65 (1). pp. 25-41. ISSN 2289-7879
  18. Afzal, Asif and A. D., Mohammad Samee and R. K., Abdul Razzak and Khan, Sher Afghan and Khan, Hurmatulla (2020) Optimum spacing between grooved tubes: an experimental study. Journal of Mechanical Science and Technology, 34 (1). pp. 469-475. ISSN 1226-4865
  19. Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2019) Estimation of stiffness derivative of an ogive for specific heat ratio 1.666. Test Engineering and Management, 81 (11-12). pp. 5091-5100. ISSN 0193-4120
  20. Mohd, Umair Siddiqui and Ansari, Emaad and Khan, Sher Afghan and Gulhane, Nitin Parashram and Patil, Rajesh (2020) Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity. Journal of Thermophysics and Heat Transfer, 34 (1). pp. 1-15. ISSN 0887-8722

Most Viewed Items

Item titleViews
1Active control of flow through the nozzles at sonic Mach number980
2Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field974
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges941
4Influence of micro jets on wall pressure for area ratio 3.24919
5The effect of micro jets on wall pressure for sonic under expanded flow905
6Studies on wall pressure flow control by micro jets for high area ratio892
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios883
8Control of suddenly expanded flow at low supersonic Mach numbers845
9Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56811
10Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge801
11Control of base pressure with micro jets for area ratio 2.4787
12Effect of level of expansion and inertia level in a suddenly expanded flow784
13Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 777
14Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow773
15Stabilty derivatives in the newtonian limit767
16Stability derivatives of a delta wing with straight leading edge in the Newtonian limit766
17An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle766
18Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges760
19Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 758
20Effect of mach number in a suddenly expanded flow for area ratio 4.84755
21Effect of mach number on wall pressure flow field for area ratio 2.56755
22Base pressure studies from over expanded nozzle for area ratio 2.56752
23Supersonic similitude for oscillating non-planar wedge749
24Control of base pressure with micro jets:part-I746
25Experimental study of suddenly expanded flow from correctly expanded nozzles741
26Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow739
27Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD733
28Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 731
29Active control of base pressure in suddenly expanded flow for area ratio 4.84726
30Combined effect of relief and level of expansion in a suddenly expanded flow719