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Prof. Dr. Sher Afghan Khan

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  1. 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
  2. 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
  3. 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
  4. 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
  5. 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
  6. Pathan, Khizar Ahmed and Syed, Ashfaq and Dabeer, Prakash S and Khan, Sher Afghan (2019) Analysis of parameters affecting thrust and base pressure in suddenly expanded flow from nozzle. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 64 (1). pp. 1-18. ISSN 2289-7879
  7. 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
  8. 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
  9. 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
  10. 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
  11. 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
  12. 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
  13. 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
  14. 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
  15. 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
  16. 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
  17. 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
  18. 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
  19. 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
  20. 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

Most Viewed Items

Item titleViews
1Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field913
2Active control of flow through the nozzles at sonic Mach number905
3Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges859
4Influence of micro jets on wall pressure for area ratio 3.24854
5The effect of micro jets on wall pressure for sonic under expanded flow844
6Studies on wall pressure flow control by micro jets for high area ratio834
7Studies on wall pressure of sonic flow through the converging nozzles for different area ratios823
8Control of suddenly expanded flow at low supersonic Mach numbers767
9Control of base pressure with micro jets for area ratio 2.4729
10Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge719
11Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 716
12Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56716
13Effect of level of expansion and inertia level in a suddenly expanded flow706
14Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow704
15Effect of mach number on wall pressure flow field for area ratio 2.56700
16Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges696
17Stabilty derivatives in the newtonian limit696
18Stability derivatives of a delta wing with straight leading edge in the Newtonian limit696
19An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle695
20Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets 692
21Supersonic similitude for oscillating non-planar wedge691
22Effect of mach number in a suddenly expanded flow for area ratio 4.84688
23Control of base pressure with micro jets:part-I681
24Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges 670
25Base pressure studies from over expanded nozzle for area ratio 2.56669
26Experimental study of suddenly expanded flow from correctly expanded nozzles663
27Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow661
28Active control of base pressure in suddenly expanded flow for area ratio 4.84658
29Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD656
30Combined effect of relief and level of expansion in a suddenly expanded flow654