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Research Article

Response surface analysis of nozzle parameters at supersonic flow through microjets

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Pages 1037-1052 | Received 31 Dec 2020, Accepted 02 Jun 2021, Published online: 28 Jun 2021

References

  • Aabid, A., A. Afifi, F. Ahmed Ghasi Mehaboob Ali, M. Nishat Akhtar, and S. Afghan Khan. 2019a. “CFD Analysis of Splitter Plate on Bluff Body.” CFD Letters, 11: 25–38
  • Aabid, A., A. Khan, N. M. Mazlan, M. A. Ismail, M. N. Akhtar, and S. A. Khan. 2019b. “Numerical Simulation of Suddenly Expanded Flow at Mach 2.2.” International Journal of Engineering and Advanced Technology 8 (3): 452–457
  • Aabid, A., S. A. Khan, M. Ahmed, A. Baig, and A. R. Reddy. 2021c. “Investigation of Flow Growth in a Duct Flows for Higher Area Ratio.” IOP Conf. Series: Materials Science and Engineering 1057 (12052): 10. doi:10.1088/1757-899X/1057/1/012052
  • Aabid, A., S. A. Khan, M. Ahmed, A. Baig, and A. R. Reddy. 2021d. “Investigation of Flow Growth in a Duct Flows for Higher Area Ratio.” IOP Conf. Series: Materials Science and Engineering, 1057 (12052): 10. doi:10.1088/1757-899X/1057/1/012052
  • Aabid, A., and S. Afghan Khan. 2021. “Determination of Wall Pressure Flows at Supersonic Mach Numbers.” Materials Today: Proceedings 38: 2347–2352. doi:10.1016/j.matpr.2020.06.538.
  • Aabid, A., and S. A. Khan. 2021a. “Investigation of High-Speed Flow Control from CD Nozzle Using Design of Experiments and CFD Methods.” Arabian Journal for Science and Engineering 46 (3): 2201–2230. doi:10.1007/s13369-020-05042-z.
  • Aabid, A., and S. A. Khan. 2021b. “Studies on Flows Development in a Suddenly Expanded Circular Duct at Supersonic Mach Numbers.” International Journal of Heat and Technology 39 (1): 185–194. doi:10.18280/ijht.390120.
  • Aabid, A., S. A. Khan, M. Ahmed, A. Baig, and A. R. Reddy. 2021d. “Investigation of Flow Growth in a Duct Flows for Higher Area Ratio.” IOP Conf. Series: Materials Science and Engineering 1057 (12052): 10. doi:10.1088/1757-899X/1057/1/012052.
  • Aabid, A., S. A. Khan, M. Ahmed, A. Baig, and K. S. Rao. 2021c. “Effect of Control on the Duct Flow at High Mach Numbers.” IOP Conf. Series: Materials Science and Engineering 1057 (12053): 9. doi:10.1088/1757-899X/1057/1/012053.
  • Aabid, Abdul, Fhrukh Ahmed G M, and Sher Afghan K. 2019. “Experimental Investigation of Wall Pressure Distribution in a Suddenly Expanded Duct from a Convergent-Divergent Nozzle”. In 2019 6th IEEE International Conference on Engineering Technologies and Applied Sciences (ICETAS), 6. https://doi.org/10.1109/ICETAS48360.2019.9117428.
  • Aabid, Abdul, Liyana Nabilah, Binti Khairulaman, and Sher Afghan K. 2021. “Analysis of Flows and Prediction of CH10 Airfoil for Unmanned Arial Vehicle Wing Design”. Advances in Aircraft and Spacecraft Science 8 (2): 24.
  • Afifi, A., A. Aabid, and S. Afghan Khan. 2021. “Numerical Investigation of Splitter Plate Effect on Bluff Body Using Finite Volume Method.” Materials Today: Proceedings 38: 2181–2190. doi:10.1016/j.matpr.2020.05.559.
  • Afzal, A., A. Aabid, A. Khan, S. A. Khan, T. Nath, and R. Kumar. 2020a. “Response Surface Analysis, Clustering, and Random Forest Regression of Pressure in Suddenly Expanded High-speed Aerodynamic Flows.” Aerospace Science and Technology 1: 106318. doi:10.1016/j.ast.2020.106318.
  • Afzal, A., S. A. Khan, M. T. Islam, R. D. Jilte, A. Khan, and M. E. M. Soudagar. 2020b. “Investigation and Back-propagation Modeling of Base Pressure at Sonic and Supersonic Mach Numbers.” Physics of Fluids 32 (9): 9. doi:10.1063/5.0022015.
  • Afzal, Asif, Sher Afghan Khan, Md Tariqul Islam, R. D. Jilte, Ambareen Khan, and Manzoore Elahi M. Soudagar. 2020b.“Investigation and Back-Propagation Modeling of Base Pressure at Sonic and Supersonic Mach Numbers.” Physics of Fluids 32 (9): 096109. https://doi.org/10.1063/5.0022015
  • Ahmed, F., and S. A. Khan. 2018. “Investigation of Efficacy of Low Length-to-diameter Ratio and Nozzle Pressure Ratio on Base Pressure in an Abruptly Expanded Flow.” MATEC Web of Conferences 01004: 1–6. doi:10.1051/matecconf/201817201004.
  • Akhtar, M. N., E. A. Bakar, A. Aabid, and S. A. Khan. 2019. “Effects of Micro Jets on the Flow Field of the Duct with Sudden Expansion.” International Journal of Innovative Technology and Exploring Engineering 8: 636–640. doi:10.35940/ijitee.I1129.0789S219.
  • Al-khalifah, T., A. Aabid, and S. A. Khan. 2020. “Regression Analysis of Flow Parameters at High Mach Numbers.” Solid State Technology 63 (6): 5473–5488.
  • Chaudhary, Z. I., V. B. Shinde, and S. A. Khan. 2018. “Investigation of Base Flow for an Axisymmetric Suddenly Expanded Nozzle with Micro JET.” International Journal of Engineering & Technology 7 (3.29): 236–242. doi:10.14419/ijet.v7i3.29.18803.
  • Faheem, M., M. Kareemullah, A. Aabid, I. Mokashi, and S. A. Khan. 2019. “Experiment on of Nozzle Flow with Sudden Expansion at Mach 1.1.” International Journal of Recent Technology and Engineering 8(2S8): 1769–1775. doi:10.35940/ijrte.B1150.0882S819.
  • Fharukh, A. G. M., A. A. Alrobaian, A. Aabid, and S. A. Khan. 2018. “Numerical Analysis of Convergent-Divergent Nozzle Using Finite Element Method.” International Journal of Mechanical and Production Engineering and Development 8 (6): 373–382. www.tjprc.org.
  • Khan, A., A. Aabid, and S. A. Khan. 2018. “CFD Analysis of Convergent-divergent Nozzle Flow and Base Pressure Control Using micro-JETS.” International Journal of Engineering & Technology 7 (3): 232. doi:10.14419/ijet.v7i3.29.18802.
  • Khan, S. A., A. Aabid, and C. A. Saleel. 2019a. “CFD Simulation with Analytical and Theoretical Validation of Different Flow Parameters for the Wedge at Supersonic Mach Number.” International Journal of Mechanical & Mechatronics Engineering 19 (1): 170–177.
  • Khan, S. A., A. Aabid, and C. A. Saleel. 2019b. “Influence of Micro Jets on the Flow Development in the Enlarged Duct at Supersonic Mach Number.” International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS 19 (1): 70–82.
  • Khan, S. A., A. Aabid, I. Mokashi, A. A. Al-Robaian, and A. S. Alsagri. 2019c. “Optimization of Two-dimensional Wedge Flow Field at Supersonic Mach Number.” CFD Letters 11: 80–97.
  • Khan, S. A., A. Aabid, I. Mokashi, and Z. Ahmed. 2019a. “Effect of Micro Jet Control on the Flow Field of the Duct at Mach 1.5.” International Journal of Recent Technology and Engineering (IJRTE) 8 (2S8): 1758–1762. doi:10.35940/ijrte.B1148.0882S819.
  • Khan, S. A., A. Aabid, and M. A. A. Baig. 2018. “CFD Analysis of Cd Nozzle and Effect of Nozzle Pressure Ratio on Pressure and Velocity for Suddenly Expanded Flows.” International Journal of Mechanical and Production Engineering Research and Development 8 (3): 1147–1158. doi:10.24247/ijmperdjun2018119.
  • Khan, S. A., A. Aabid, and Z. I. Chaudhary. 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 8 (6S4): 1135–1138. 6 Special Issue 4. doi:10.35940/ijitee.F1236.0486S419.
  • Khan, Sher Afghan, Abdul Aabid, Fharukh Ahmed G M, Abdulrahman Abdullah Al-Robaian, and Ali Sulaiman Alsagri. 2019. “Analysis of Area Ratio in a CD Nozzle with Suddenly Expanded Duct Using CFD Method.” CFD Letters 11 (5): 61–71.
  • Khan, S. A., and E. Rathakrishnan. 2002a. “Active Control of Suddenly Expanded Flows from Overexpanded Nozzles.” International Journal of Turbo and Jet Engines 19 (1–2): 119–126. doi:10.1515/TJJ.2002.19.1-2.119.
  • Khan, S. A., and E. Rathakrishnan. 2002b. “Active Control of Suddenly Expanded Flows from Overexpanded Nozzles.” International Journal of Turbo and Jet Engines 19 (1–2): 119–126. doi:10.1515/TJJ.2002.19.1-2.119.
  • Khan, S. A., and E. Rathakrishnan. 2003. “Control of Suddenly Expanded Flows with Micro-Jets.” International Journal of Turbo and Jet Engines 20 (1): 63–82. doi:10.1515/TJJ.2003.20.1.63.
  • Khan, S. A., and E. Rathakrishnan. 2004a. “Active Control of Suddenly Expanded Flows from Underexpanded Nozzles.” International Journal of Turbo and Jet Engines 21: 233–254. doi:10.1515/TJJ.2004.21.4.233.
  • Khan, S. A., and E. Rathakrishnan. 2004b. “Control of Suddenly Expanded Flows from Correctly Expanded Nozzles.” International Journal of Turbo and Jet Engines 21: 255–278. doi:10.1515/TJJ.2004.21.4.255.
  • Khan, S. A., and E. Rathakrishnan. 2005. “Active Control of Suddenly Expanded Flows from Underexpanded Nozzles - Part II.” International Journal of Turbo and Jet Engines 22 (3): 163–183. doi:10.1515/TJJ.2005.22.3.163.
  • Khan, S. A., and E. Rathakrishnan. 2006. “Reattachment Point Recirculation.” International Journal of Turbo and Jet Engines 23: 233–257.
  • Khan, S. A., I. Mokashi, A. Aabid, and M. Faheem. 2019b. “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): 971–975. doi:10.35940/ijrte.B1182.0782S319.
  • Khan, S. A., M., . C. Mohiuddin, A. S., and M. F. G. 2019e. “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 8 (3): 570–578.
  • Kharulaman, Liyana, Abdul Aabid, Fharukh Ahmed, Ghasi Mehaboobali, and Sher Afghan Khan. 2019. “Research on Flows for NACA 2412 Airfoil Using Computational Fluid Dynamics Method.” International Journal of Engineering and Advanced Technology 9 (1): 5450–56. https://doi.org/10.35940/ijeat.A3085.109119 .
  • Quadros, J. D., S. A. Khan, S. Sapkota, J. Vikram, and T. Prashanth. 2020. “On Recirculation Region Length of Suddenly Expanded Supersonic Flows, Using CFD and Fuzzy Logic.” International Journal of Computational Fluid Dynamics 1–16. doi:10.1080/10618562.2020.1828580.
  • Sajali, M. F. M., A. Aabid, S. A. Khan, F. A. G. Mehaboobali, and E. Sulaeman. 2019a. “Numerical Investigation of Flow Field of a Non-circular Cylinder.” CFD Letters 11 (5): 37–49.
  • Sajali, M. F. M., S. Ashfaq, A. Aabid, and S. A. Khan. 2019b. “Simulation of Effect of Various Distances between Front and Rear Body on Drag of a Non-Circular Cylinder.” Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 62 (1): 53–65.
  • Vijayaraja, K., C. Senthilkumar, S. Elangovan, and E. Rathakrishnan. 2014. “Base Pressure Control with Annular Ribs.” International Journal of Turbo and Jet Engines 31 (2): 111–118. doi:10.1515/tjj-2013-0037.
  • Vikramaditya, N. S., M. Viji, and S. B. Verma. 2017. “Base Pressure Fluctuations on Typical Missile Configuration in Presence of Base Cavity.” JOURNAL OF SPACECRAFT AND ROCKETS 1–11. doi:10.2514/1.A33926.

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