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Prof. Dr. Sher Afghan Khan

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  1. Aabid, Abdul and Khan, Sher Afghan and Baig, Maugal Ahmed Ali and Rao, K Srinivasa (2021) Effect of control on the duct flow at high mach numbers. Material Science, 1057. pp. 1-10. ISSN 1757-899X
  2. Aabid, Abdul and Khan, Sher Afghan and Baig, Maugal Ahmed Ali and Reddy, Avala Raji (2021) Investigation of flow growth in a duct flows for higher area ratio. Materials Science and Engineering, 1057. pp. 1-11. ISSN 1757-8981 E-ISSN 1757-899X
  3. Akhtar, Mohammad Nishat and Khan, Sher Afghan and Mohamed, Mazlan and Janvekar, Ayub (2020) Automated image analysis and improvisations to manage palm oil plantation. In: 3rd Tarumanagara International Conference of the Applications of Technology and Engineering (TICATE), 3-4 August 2020, Jakarta, Indonesia.
  4. Faheem, Mohammed and Khan, Aqib and Kumar, Rakesh and Khan, Sher Afghan and Asrar, Waqar and Sapardi, Azan M. (2021) Experimental study on the mean flow characteristics of a supersonic multiple jet configuration. Journal of Aerospace Science & Technology, 108 (2021). pp. 1-13. ISSN 1270-9638 E-ISSN 1626-3219
  5. Mokashi, Imran and Afzal, Asif and Khan, Sher Afghan and Abdullah, Nur Azam and Azami, Muhammad Hanafi and Jilte, Ravindra D. and Samuel, Olusegun David (2020) Nusselt number analysis from a battery pack cooled by different fluids and multiple back-propagation modelling using feed-forward networks. International Journal of Thermal Science. pp. 1-20. ISSN 1290-0729 (In Press)
  6. Afzal, Asif and Mokashi, Imran and Khan, Sher Afghan and Abdullah, Nur Azam and Azami, Muhammad Hanafi (2020) Optimization 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 algorithm. Numerical Heat Transfer, Part A: Applications. ISSN 1521-0634 E-ISSN 1040-7782 (In Press)
  7. Al-Ghurabi, Ebrahim H. and Asif, Mohammad and Siva Kumar, Nadavala and Khan, Sher Afghan (2020) Fluidization dynamics of hydrophobic nanosilica with velocity step changes. Applied Sciences, 10 (22). pp. 1-12. ISSN 2076-3417
  8. 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)
  9. 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
  10. 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
  11. 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
  12. Khan, Sher Afghan and Siddique, Umair M and Ansari, Emaad and Patil, Rajesh (2020) Numerical investigation of semi-empirical relation representing standard deviation in Nusselt profile due to water jet impingement. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 65 (1). pp. 42-53. ISSN 2289-7879
  13. 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)
  14. 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)
  15. 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
  16. 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
  17. 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
  18. 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 (6). pp. 2555-2571. ISSN 1388-6150 E-ISSN 1588-2926
  19. 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
  20. 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

Most Viewed Items

Item titleViews
1Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field1113
2Active control of flow through the nozzles at sonic Mach number1109
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges1085
4Studies on wall pressure flow control by micro jets for high area ratio1042
5Influence of micro jets on wall pressure for area ratio 3.241038
6The effect of micro jets on wall pressure for sonic under expanded flow1037
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios1026
8Control of suddenly expanded flow at low supersonic Mach numbers970
9Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56969
10Control of base pressure with micro jets for area ratio 2.4942
11Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge941
12Effect of level of expansion and inertia level in a suddenly expanded flow922
13Stabilty derivatives in the newtonian limit913
14An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle908
15Stability derivatives of a delta wing with straight leading edge in the Newtonian limit905
16Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 904
17Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 901
18Base pressure studies from over expanded nozzle for area ratio 2.56896
19Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges893
20Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow891
21Experimental study of suddenly expanded flow from correctly expanded nozzles889
22Control of base pressure with micro jets:part-I888
23Effect of mach number on wall pressure flow field for area ratio 2.56886
24Supersonic similitude for oscillating non-planar wedge883
25Effect of mach number in a suddenly expanded flow for area ratio 4.84875
26Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD869
27Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 856
28Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow855
29Active control of base pressure in suddenly expanded flow for area ratio 4.84854
30Combined effect of relief and level of expansion in a suddenly expanded flow837