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Prof. Dr. Sher Afghan Khan

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Latest Additions

  1. Akhtar, Mohammad Nishat and Abu Bakar, Elmi and Aabid, Abdul and Khan, Sher Afghan (2019) Effects of micro jets on the flow field of the duct with sudden expansion. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (9S2). pp. 636-640. E-ISSN 2277-3075
  2. Akhtar, Mohammad Nishat and Abu Bakar, Elmi and Aabid, Abdul and Khan, Sher Afghan (2019) Control of CD nozzle flow using microjets at Mach 2.1. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (9S2). pp. 631-635. ISSN 2278-3075
  3. Akhtar, Mohammad Nishat and Abu Bakar, Elmi and Aabid, Abdul and Khan, Sher Afghan (2019) Numerical simulations of a CD nozzle and the influence of the duct length. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (9S2). pp. 622-630. ISSN 2278-3075
  4. Butt, Mohammad Mursaleen and Ahmad, Sheikh Nazir and Al-Robian, Abdulrehman A and Khan, Sher Afghan (2019) Finite element modeling and analysis of a debonded smart beam in actuation. International Journal of Recent Technology and Engineering (IJRTE), 7 (6S). pp. 258-263. ISSN 2277-3878
  5. Sethuraman, Vigneshvaran and Rajendran, Parvathy and Khan, Sher Afghan (2019) A cost-effective data acquisition instrumentation for measurement of base pressure and wall pressure in suddenly expanded flow through ducts. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 60 (1). pp. 112-123. E-ISSN 2289-7879
  6. Khan, Sher Afghan and Mokashi, Imran and Aabid, Abdul and Faheem, Mohammad (2019) Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24. International Journal of Recent Technology and Engineering, 8 (2S3). pp. 971-975. E-ISSN 2277-3878
  7. G. M., Fharukh Ahmed and Khan, Sher Afghan (2019) Effect of area ratio on base pressure and control effectiveness. International Journal of Recent Technology and Engineering, 8 (2S3). pp. 953-958. E-ISSN 2277-3878
  8. G. M, Fharukh Ahmed and Khan, Sher Afghan (2019) Role of active control in increasing base pressure at Sonic Mach Number. International Journal of Recent Technology and Engineering, 8 (2S3). pp. 966-970. E-ISSN 2277-3878
  9. Monis, Renita Sharon and Shabana, Aysha and Crasta, Asha and Khan, Sher Afghan (2019) Effect of sweep angle and a half sine wave on roll damping derivative of a Delta Wing. International Journal of Recent Technology and Engineering, 8 (2S3). pp. 984-989. E-ISSN 2277-3878
  10. Quadros, Jaimon Dennis and Khan, Sher Afghan (2020) Prediction of base pressure in a suddenly expanded flow the processes 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
  11. G M, Fharukh and Khan, Sher Afghan (2019) Control of nozzle flow using microjets at supersonic Mach Regime. International Journal of Engineering, 32 (7). pp. 991-998. ISSN 1025-2495 E-ISSN 1735-9244
  12. Khan, Sher Afghan and Aabid, Abdul and Chaudhary, Zakir Ilahi (2019) Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (6S4). pp. 1135-1138. ISSN 2278-3075
  13. Mohd Umair, Siddique and Ansari, Emad and Khan, Sher Afghan and Alrobaian, Abdulrahman (2019) On numerical investigation of semi-empirical relation representing development length for a fluid flow in a closed conduit. CFD Letters, 11 (6). pp. 63-71. E-ISSN 2180-1363
  14. Renita, Sharon Monis and Crasta, Asha and Khan, Sher Afghan (2019) Evaluation of stiffness derivative for a delta wing with straight leading edges in unsteady flow. International Journal of Engineering and Advanced Technology (IJEAT), 8 (3S). pp. 754-762. ISSN 2249 – 8958
  15. Khan, Sher Afghan and Asadullah, Mohammad and G.M, Fharukh Ahmed. and Jalaluddeen, Ahmed and Baig, Maughal Ahmed Ali (2018) Flow control with aerospike behind bluff body. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (3). pp. 1001-1008. ISSN 2249-6890 E-ISSN 2249-8001
  16. Pathan, Khizer Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2019) Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows. Journal of Applied Fluid Mechanics, 12 (4). pp. 1127-1135. ISSN 1735-3572 E-ISSN 1735-3645
  17. Asadullah, Mohammed and Khan, Sher Afghan and Soudagar, Manzoore Elahi M and T. R., Vaishak (2019) A comparison of the effect of single and multiple cavities on base flows. In: 5th IEEE International Conference on Engineering Technologies and Applied Sciences (ICETAS) 2018, 22nd-23rd Nov. 2018, Bangkok, Thailand.
  18. S, Parashurama and Saleel, C. Ahmed and M. S., Govindegowda and Khan, Sher Afghan (2019) Hydrocarbons as alternative refrigerants in domestic refrigerators. International Journal of Innovative Technology and Exploring Engineering (IJITEE), 8 (6S3). pp. 496-501. ISSN 2278-3075
  19. Warimani, Mohammadsalman and Azami, Muhammad Hanafi and Khan, Sher Afghan (2019) Challenges and solutions for using liquid fuels in aviation industry. International Journal of Engineering and Advanced Technology (IJEAT), 8 (2s2). pp. 288-290. ISSN 2249–8958
  20. Pathan, Khizar Ahmed and Dabeer, Prakash S and Khan, Sher Afghan (2019) Influence of expansion level on base pressure and reattachment length. CFD Letters, 11 (5). pp. 22-36. ISSN 2180-1363

Most Viewed Items

Item titleViews
1Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field852
2Active control of flow through the nozzles at sonic Mach number831
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges791
4Influence of micro jets on wall pressure for area ratio 3.24782
5Studies on wall pressure flow control by micro jets for high area ratio778
6The effect of micro jets on wall pressure for sonic under expanded flow769
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios744
8Control of suddenly expanded flow at low supersonic Mach numbers698
9Control of base pressure with micro jets for area ratio 2.4669
10Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 654
11Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge649
12Effect of level of expansion and inertia level in a suddenly expanded flow643
13Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow640
14Effect of mach number on wall pressure flow field for area ratio 2.56638
15Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56634
16An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle630
17Effect of mach number in a suddenly expanded flow for area ratio 4.84623
18Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges623
19Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 621
20Supersonic similitude for oscillating non-planar wedge620
21Stability derivatives of a delta wing with straight leading edge in the Newtonian limit619
22Stabilty derivatives in the newtonian limit612
23Control of base pressure with micro jets:part-I611
24Base pressure studies from over expanded nozzle for area ratio 2.56604
25Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 602
26Experimental study of suddenly expanded flow from correctly expanded nozzles599
27Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow593
28Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD590
29Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge590
30Active control of base pressure in suddenly expanded flow for area ratio 4.84589