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Prof. Dr. Sher Afghan Khan

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  1. Aabid, Abdul and Afifi, Azmil and Mehaboobali, Fharukh Ahmed Ghasi and Akhtar, Mohammad Nishat and Khan, Sher Afghan (2019) CFD analysis of splitter plate on bluff body. CFD Lettrs, 11 (11). pp. 25-38. ISSN 2180-1363
  2. Aabid, Abdul and Chaudhary, Zakir Ilahi and Khan, Sher Afghan (2019) Modeling 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 E-ISSN 2289-7879
  3. Mohd Zakuan, Muhammad Amir Mirza and Aabid, Abdul and Khan, Sher Afghan (2019) Modeling and structural analysis of three-dimensional wing. International Journal of Engineering and Advanced Technology (IJEAT), 9 (1). pp. 6820-6828. ISSN 2249-8958
  4. Renita, sharon Monis and Crasta, Asha and Faheem, Mohammed and Khan, Sher Afghan (2019) Analysis of damping derivatives for delta wings in hypersonic flow for curved leading edges with full sine wave. International Journal of Engineering and Advanced Technology (IJEAT), 9 (1). pp. 5457-5466. ISSN 2249-8958
  5. Kharulaman, Liyana and Aabid, Abdul and Mehaboobali, Fharukh Ahmed Ghasi and Khan, Sher Afghan (2019) Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method. International Journal of Engineering and Advanced Technology (IJEAT), 9 (1). pp. 5450-5456. ISSN 2249 – 8958
  6. Afzal, Asif and Khan, Sher Afghan and Saleel, Ahmed (2019) Role of ultrasonication duration and surfactant on characteristics of ZnO and CuO nanofluids. Materials Research Express, 6 (11). pp. 1-13. ISSN 2053-1591 E-ISSN 2053-1591
  7. Delvi, Hamza Afser and Faheem, Mohammed and Khan, Sher Afghan and Kumar M., Kiran and Kareem Ullah, Mohammad (2019) Effect of ethanol-gasoline blends on performance, combustion and emission characteristics of spark ignition engine. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 62 (2). pp. 209-220. ISSN 2289-7879
  8. Sajali, Muhammad Fahmi Mohd and Syed, Ashfaq and Aabid, Abdul and Khan, Sher Afghan (2019) Simulation of effect of various distances between front and rear body on drag of a non-circular cylinder. Advanced Research in Fluid Mechanics and Thermal Sciences, 62 (1). pp. 53-65. ISSN 2289-7879
  9. Renita, sharon Monis and Crasta, Asha and Khan, Sher Afghan (2019) Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge. International Journal of Mechanical and Production Engineering Research and Development, 9 (5). pp. 255-264. ISSN 2249-6890 E-ISSN 2249-8001
  10. Umair, Siddiqui and Ansari, Emad and Khan, Sher Afghan and Patil, Rajesh (2019) On numerical investigation of nusselt distribution profile of heat sink using lateral impingement of air jet. CFD Letters, 11 (9). pp. 59-68. ISSN 2180-1363
  11. Faheem, Mohammad and Kareem Ullah, Mohammad and Aabid, Abdul and Mokashi, Imran and Khan, Sher Afghan (2019) Experiment on of nozzle flow with sudden expansion at Mach 1.1. International Journal of Recent Technology and Engineering (IJRTE), 8 (2S8). pp. 1769-1775. E-ISSN 2277-3878
  12. Khan, Sher Afghan and Ahmad, Zaheer and Aabid, Abdul and Mokashi, Imran (2019) Experimental research on flow development and control effectiveness in the duct at high speed. International Journal of Recent Technology and Engineering (IJRTE), 8 (2S8). pp. 1763-1768. E-ISSN 2277-3878
  13. Khan, Sher Afghan and Aabid, Abdul and Mokashi, Imran and Ahmad, Zaheer (2019) Effect of micro jet control on the flow filed of the duct at Mach 1.5. International Journal of Recent Technology and Engineering (IJRTE), 8 (2S8). pp. 1758-1762. E-ISSN 2277-3878
  14. 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
  15. 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
  16. 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
  17. 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
  18. 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
  19. 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
  20. 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

Most Viewed Items

Item titleViews
1Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field875
2Active control of flow through the nozzles at sonic Mach number861
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges820
4Influence of micro jets on wall pressure for area ratio 3.24807
5Studies on wall pressure flow control by micro jets for high area ratio802
6The effect of micro jets on wall pressure for sonic under expanded flow797
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios776
8Control of suddenly expanded flow at low supersonic Mach numbers725
9Control of base pressure with micro jets for area ratio 2.4695
10Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge682
11Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 678
12Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56671
13Effect of level of expansion and inertia level in a suddenly expanded flow670
14Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow669
15Effect of mach number on wall pressure flow field for area ratio 2.56662
16An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle659
17Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges653
18Effect of mach number in a suddenly expanded flow for area ratio 4.84651
19Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 651
20Stability derivatives of a delta wing with straight leading edge in the Newtonian limit650
21Stabilty derivatives in the newtonian limit649
22Supersonic similitude for oscillating non-planar wedge646
23Base pressure studies from over expanded nozzle for area ratio 2.56640
24Control of base pressure with micro jets:part-I638
25Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 627
26Experimental study of suddenly expanded flow from correctly expanded nozzles627
27Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD623
28Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow621
29Combined effect of relief and level of expansion in a suddenly expanded flow616
30Active control of base pressure in suddenly expanded flow for area ratio 4.84616