IIUM Repository (IREP)

Prof. Dr. Sher Afghan Khan

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  1. Aabid, Abdul and Khan, Ambareen and Mazlan, Nur Musfira and Ismail, Mohd Azmi and Akhtar, M. Nishat and Khan, Sher Afghan (2019) Numerical simulation of suddenly expanded flow at Mach 2.2. International journal of Engineering & Advanced Technology (IJEAT), 8 (3). pp. 457-462. ISSN 2249-8958
  2. Khan, Sher Afghan and Mohiuddin, A K M and Saleel, Ahmad C and G M, Fharukh (2019) Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles. International Journal of Engineering and Advanced Technology (IJEAT), 8 (3). pp. 570-578.
  3. Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2019) An effect of sweep angle on roll damping derivative for a Delta wing with curved leading edges in unsteady flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 9 (2). pp. 361-373. ISSN 2249-6890
  4. Hamizi, Ilya Bashiera and Khan, Sher Afghan (2019) Aerodynamics investigation of delta wing at low Reynold’s number. CFD letters, 11 (2). pp. 32-41. ISSN 2180-1363
  5. Saleel, Ahmed and Baig, Maughal Ahmed Ali and Khan, Sher Afghan (2018) Experimental investigation of the base flow and base pressure of sudden expansion nozzle. In: International Conference on Aerospace and Mechanical Engineering (AeroMech17), 21st-22nd November 2017, Batu Ferringhi, Penang.
  6. Siddique, Mohd Umair and Gulhane, N P and Al-Robaian, Abdul Rehman A and Khan, Sher Afghan (2019) On numerical investigation of semi-empirical relations representing local nusselt number at lower nozzle-target spacing’s. International Journal of Engineering, 32 (1). pp. 137-145. ISSN 1025-2495
  7. Khan, Sher Afghan and Alrobaian, Abdul Rahman and Asad Ullah, Mohammed and Rao, Ashwin (2019) Threaded spikes for bluff body base flow control. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 53 (2). pp. 194-203.
  8. Khan, Sher Afghan and Alrobaian, Abdul Rahman and Asad Ullah, Mohammed and Khan, Abdul Mohsin (2019) Grooved cavity as a passive controller behind backward facing step. International Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 53 (2). pp. 185-193. ISSN 2289-7879
  9. Mohammed Umair, Siddque and Alrobaian, Abdul Rahman and Khan, Sher Afghan and Gnanagonda Kashinath, Marthande and Rajesh, Patil (2018) Numerical investigation of critical range for the occurrence of secondary peaks in the Nusselt distribution curve. CFD Letters, 10 (2). pp. 1-17. ISSN 2180-1363
  10. Al-Robaian, Abdul Rehman A and Khan, Sher Afghan and Asad Ullah, Mohammed and G. M., Fharrukh Ahmed and Imtiyaz, A (2018) A new approach to low-cost open-typed subsonic compressible flow wind tunnel for academic purpose. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (6). pp. 383-394. ISSN 2249-6890
  11. G M, Fharukh Ahmed and Al-Robaian, Abdul Rehman A and Aabid, Abdul and Khan, Sher Afghan (2018) Numerical analysis of convergent-divergent nozzle using finite element method. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (6). pp. 373-382. ISSN 2249-6890
  12. Pathan, Khizer Ahmed and Dabeer, P S and Khan, Sher Afghan (2018) An investigation to control base pressure in suddenly expanded flows. International Review of Aerospace Engineering (IREASE), 11 (4). pp. 162-169. ISSN 1973-7459
  13. Asadullah, Mohammed and Khan, Sher Afghan and Asrar, Waqar (2018) Active control of base pressure with counter clockwise rotating cylinder at Mach 2. In: 4th IEEE International Conference on Engineering Technologies and Applied Sciences, ICETAS 2017, 29 November - 1 December 2017, AMA International University Salmabad; Bahrain.
  14. Khan, Sher Afghan and Riyadh, MiahMohammed and Ibrahim, Mir Owais Ali and Elrashid, Yousof and Arefin, Nafis Mahdi and Kabir, Shahriar and G M, Fharukh Ahmed (2018) Design & development of a gravity powered fan using gear transmission. International Journal of Engineering & Technology, 7 (3.29 (Special issue 29)). pp. 632-637. ISSN 2227-524X
  15. Ahmed, Fharrukh and Khan, Sher Afghan (2018) Investigation of efficacy of low length-to-diameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow. In: 3rd International Conference on Design, Analysis, Manufacturing and Simulation, ICDAMS 2018, 6 - 7 April 2018, Chennai, Tamilnadu; India.
  16. Pathan, Khizer Ahmed and Dabeer, P. S. and Khan, Sher Afghan (2018) Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers. Case Study in Thermal Engineering, 12. pp. 696-700. ISSN 2214-157X
  17. Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2018) Estimation of stability derivatives in newtonian limit for oscillating cone. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21-22 November 2017, Parkroyal HotelBatu Ferringhi, Penang; Malaysia.
  18. Aabid, Abdul and Khan, Sher Afghan (2018) Design and fabrication of flying saucer utilizing coanda effect. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21 - 22 November 2017, Parkroyal HotelBatu Ferringhi, Penang; Malaysia.
  19. Asadullah, Mohammed and Khan, Sher Afghan and Asrar, Waqar and Sulaeman, Erwin (2018) Counter clockwise rotation of cylinder with variable position to control base flows. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21 - 22 November 2017, Parkroyal HotelBatu Ferringhi, Penang; Malaysia.
  20. Shabana, Aysha and Monis, Renita Sharon and Crasta, Asha and Khan, Sher Afghan (2018) Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66. In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017, 21 - 22 November 2017, Parkroyal HotelBatu Ferringhi, Penang.

Most Viewed Items

Item titleViews
1Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field765
2Active control of flow through the nozzles at sonic Mach number749
3Influence of micro jets on wall pressure for area ratio 3.24703
4Studies on wall pressure flow control by micro jets for high area ratio699
5Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges694
6The effect of micro jets on wall pressure for sonic under expanded flow683
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios665
8Control of suddenly expanded flow at low supersonic Mach numbers620
9Control of base pressure with micro jets for area ratio 2.4591
10Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 577
11Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge567
12Effect of mach number on wall pressure flow field for area ratio 2.56563
13Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow556
14Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56555
15Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges547
16Supersonic similitude for oscillating non-planar wedge545
17Effect of level of expansion and inertia level in a suddenly expanded flow538
18Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 537
19An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle537
20Base pressure studies from over expanded nozzle for area ratio 2.56534
21Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 532
22Experimental study of suddenly expanded flow from correctly expanded nozzles528
23Stabilty derivatives in the newtonian limit527
24Stability derivatives of a delta wing with straight leading edge in the Newtonian limit526
25Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow525
26Effect of mach number in a suddenly expanded flow for area ratio 4.84520
27Control of base pressure with micro jets:part-I520
28Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD520
29Active control of base pressure in suddenly expanded flow for area ratio 4.84517
30Combined effect of relief and level of expansion in a suddenly expanded flow515