ADVANCED PROPULSION TECH LAB

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JOURNALS

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Journals:

  1. 1. Baskaran SP, Muruganandam TM. A study on shock-wave/boundary-layer interaction with varying flow deflection angle. Physics of Fluids. 2024 May 1;36(5). Click here
  2. 2. Sebastian DS, Muruganandam TM. Transition of Edney shock–shock interactions due to the whipping phenomenon of liquid jet in supersonic crossflow. Physics of Fluids. 2024 Feb 1;36(2).
  3. 3. Krishnasamy Bharathi, A., Shrivastava, P., Srivatsav, H., T. M. M., and K., V. (February 27, 2023). "Investigation of Soot in a Model CFM56 Atmospheric Combustor Using In-Situ Laser-Induced Incandescence Calibration." ASME. J. Eng. Gas Turbines Power. July 2023; 145(7): 071002.Click here
  4. 4. Rocky Simon Pinto, T. Sree Renganathan, S. M. D. Hamid Ansari, and T. M. Muruganandam, “Effects of stagnation temperature on hysteresis in flame stabilization in a hydrogen-fueled strut-stabilized supersonic combustor”, International Journal of Hydrogen Energy, Available online May 2023. Click here
  5. 5. Sarath, P., and Muruganandam, T. M. (2023). "Numerical Investigation on the Characteristics of a Novel Multi-Swirl Lean Direct Injection Burner With Large Eddy Simulation-Flamelet Generated Manifold Method." ASME. J. Eng. Gas Turbines Power. July 2023; 145(7): 071006. Click here
  6. 6. Rocky Simon Pinto, T. Sree Renganathan, S. M. D. Hamid Ansari, and T. M. Muruganandam, “Hysteresis in flame stabilization in a hydrogen fueled supersonic combustor,” International Journal of Hydrogen Energy, Jun. 2022.Click here
  7. 7. A.A. Dhankarghare, T. Jayachandran, T.M. Muruganandam, “Comparative investigation of strut cavity and wall cavity in supersonic flows”, Aerospace Science and Technology, Vol.124, 107520, Mar 2022.Click here
  8. 8. Bhavya Naidu Panduri and T.M. Muruganandam, “Four-Wall Flow Separation Control Using Microvortex Generators in Supersonic Duct”, AIAA Jl., Vol. 60, No. 2, Feb 2022, pp. 1-11.Click here
  9. 9. V. I. Yazhini, Balusamy Kathiravan, T. M. Muruganandam, and Kandasamy Jayaraman, “Cowl Length Variation on Performance Characteristics of a Single Expansion Ramp Nozzle”, Jl. Prop. Power, Vol. 37, No. 5, Sep 2021, pp.780-791. Click here
  10. 10. Surya P. Baskaran and T.M. Muruganandam, “Influence of Finite Width of Shock Generator on Shock-Wave/Boundary-Layer Interaction”, AIAA Jl., Vol. 59, No. 9, Sep 2021, pp. 3387-3397. Click here
  11. 11. Vaisakh S., T. M. Muruganandam, “Visualisation of over-expanded supersonic wall jet”, Aerospace Science and Technology, Vol 112, No. 106617, Feb 2021. Click here
  12. 12. Arefyev, K.Y., Guskov, O.V., Prokhorov, A.N., Saveliev, A.S., Son, E.E., Gautham, K., Sam, D., Sonu, K.T., Muruganandam, T.M., “Experimental Research of Gasdynamic Liquid Drops Breakup in the Supersonic Flow with an Oblique Shock Wave”, High Temperature, Vol. 58, pp. 884–892, Dec 2020. Click here
  13. 13. Saravanan R, S. L. N. Desikan and Muruganandam TM., “Isolator characteristics under steady and oscillatory back pressures”, Physics of Fluids, Volume 32, Issue 9, article id.096104, Sep 2020. Click here
  14. 14. K. Sathiyamoorthy, Tahzeeb H. Danish., Venkat S. Iyengar., J. Srinivas, X. Harikrishna, T.M. Muruganandam, and Chakravarthy, S.R, "Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow", Jl. Prop. Power, Vol. 36, Nov 2020, pp. 920-930. Click here
  15. 15. Vaisakh S., T.M. Muruganandam, "Affordable schlieren visualization methods for understanding three-dimensional supersonic flows", Jl. Visualisation, Oct 2020, 23:851–862, Pulished online Jun 2020.Click here
  16. 16. Sathiyamoorthy, K, Tahzeeb Hassan Danish, Pratheesh Kumar P, Venkat S Iyengar, Manjunath P., T. M. Muruganandam, and S.R. Chakravarthy, "Flow visualization and supersonic combustion studies of an acoustically open strut cavity", Acta Astronautica, Vol. 175, Oct 2020, pp. 128-141. Click here
  17. 17. P. Senthilkumar and T.M. Muruganandam, "Numerical Simulation of Supersonic Flow through Scramjet Intake with Concavity in Cowl Surface", Journal of Applied Fluid Mechanics, Vol. 13, No. 5, Sep 2020, pp. 1601-1610, 2020. Click here
  18. 18. Sonu K. Thomas, Akash B. and Thiruchengode. M. Muruganandam, "Multistaging of Nonuniform Area Resonator based Fluidic Acoustic Pump", Sensors and Actuators A: Physical, Volume 301, 1 Jan 2020, 111751. Click here
  19. 19. S. Manoj Prabakar, Lakhan M. Panchabudhe, T.M. Muruganandam, and T.Sundararajan, " A study on the performance characteristics of two-stream supersonic diffusers", Aerospace Sci. Tech., Vol. 95, Dec 2019, 105470, Click here
  20. 20. Vaisakh S, Namratha P. R. and T. M. Muruganandam, "Effect of duct aspect ratio on normal shock wave boundary layer interaction", Technical Note, Shock Waves, Vol. 30, Oct 2019, pp. 215-219, doi:10.1007/s00193-019-00929-9.
  21. 21. S Vaisakh, TM Muruganandam, "Influence of multi-wall separation control on normal-shock-induced separation in supersonic duct flows", Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 233, No. 9, 2019, pp. 3184-3192. Click here
  22. 22. Vinothkumar,A., Ramprakash,A., Pankaj,P., Vaibhav,T., and Muruganandam,T.M., “Simultaneous TR-SPIV and CH* Chemiluminescence during precursor to LBO in a Lean Premixed Swirl Dump Combustor,” presented in Combustion Symposium 2018, Proceedings of the Combustion Institute, Vol. 37, No. 4, 2019, pp. 5105-5112.Click here
  23. 23. Sonu K. Thomas and Thiruchengode. M. Muruganandam, "A review of acoustic compressors and pumps from fluidics perspective", Sensors and Actuators A: Physical, Vol. 283, No.1, Nov 2018, pp. 42-53. Click here
  24. 24. Nikhil V.V., Abhilash Nair, Niketh P, Amit Kumar, Muruganandam T.M., " The 2.5 s Microgravity Drop Tower at National Centre for Combustion Research and Development (NCCRD), Indian Institute of Technology Madras", Microgravity Sci. Technol. (2018) 30(5): 663-673. Click here
  25. 25. R.V.K. Chakravarthy, Vedanth Nair, T. M. Muruganandam and Santanu Ghosh, “Analytical and Numerical Study of Normal Shock Response in a Uniform Duct”, Physics of Fluids, Vol 30, 086101 (2018); Click here
    26. (Citations: 3)
  26. 26. Vaisakh S and T M Muruganandam, “Schlieren Measurement of 'normal-spanwise length' of a bifurcated Normal Shock Wave in a rectangular duct”, Experimental Thermal and Fluid Science, 2018, 96, pp. 43-47. Click here
    27. (Citations: 1)
  27. 27. Saravanan R., S.L.N. Desikan, and T.M. Muruganandam, "Effect of back pressure and free stream dynamic pressure on a typical ramjet engine duct under realistic supersonic inlet condition", The Aeronautical Journal, Vol. 122, No. 1247, Jan 2018, pp. 83-103. Click here
  28. 28. Sonu K. Thomas and T.M. Muruganandam, "Non-uniform Resonator based valve-less standing wave suction pump for gases", Sensors and Actuators A: Physical, Vol. 261C, 1 July 2017, pp. 40-48.
  29. 29. Sumit Sarma, A. Chakraborty, N.M. Manu, T.M. Muruganandam, V. Raghavan, S. R. Chakravarthy, "Spatio-temporal structure of vertically spreading flame over non-planar PMMA surfaces", Proceedings of the Combustion Institute, Vol. 36, No. 2, 2017, pp. 3027-3035, Click here
    30. (Citations: 1)
  30. 30. Siddharth Ahuja; and T. M. Muruganandam, "Study of Unsteady Behaviour of Dynamic Shock Systems in Supersonic Engine Intakes", World Academy of Science, Engineering and Technology International Journal of Aerospace and Mechanical Engineering, (open access) Vol:11, No:6, 2017, Click here