Influence of Finite Width of Shock Generator on Shock-Wave/Boundary-Layer Interaction von Baskaran, Surya Prakash, Muruganandam, T. M

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Isolator characteristics under steady and oscillatory back pressures von R., Saravanan, Desikan, S. L. N., T. M., Muruganandam

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Cowl Length Variation on Performance Characteristics of a Single Expansion Ramp Nozzle von Yazhini, V. I, Kathiravan, Balusamy, Muruganandam, T. M, Jayaraman, Kandasamy

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Effect of Trailing Ramp Angles in Strut-Based Injection in Supersonic Flow von Sujith, S, Muruganandam, T. M, Kurian, Job

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Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow von Sathiyamoorthy, K, Danish, Tahzeeb H, Iyengar, Venkat S, Srinivas, J, Harikrishna, X, Muruganandam, T. M, Chakravarthy, S. R

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Numerical Simulation of Supersonic Flow through Scramjet Intake with Concavity in Cowl Surface von Senthilkumar, P, Muruganandam, T M

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Influence of multi-wall separation control on normal-shock-induced separation in supersonic duct flows von Vaisakh, S, Muruganandam, TM

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A study on shock-wave/boundary-layer interaction with varying flow deflection angle von Baskaran, Surya Prakash, Muruganandam, T. M.

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Resonant Gas Oscillations in a Linear Area Variation Cavity: Rectangular Versus Circular Cross Section von Thomas, Sonu K, Muruganandam, T. M

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Effect of Flap Deflection on Single-Expansion-Ramp Nozzles Performance at Different Pressure Ratios von Srinivasan, Priyadharshini, Muruganandam, T. M., Balusamy, Kathiravan

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A twin unidirectional impulse turbine topology for OWC based wave energy plants – Experimental validation and scaling von Mala, K., Jayaraj, J., Jayashankar, V., Muruganandam, T.M., Santhakumar, S., Ravindran, M., Takao, M., Setoguchi, T., Toyota, K., Nagata, S.

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Transition of Edney shock–shock interactions due to the whipping phenomenon of liquid jet in supersonic crossflow von Sebastian, Dominic S., Muruganandam, T. M.

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A numerical investigation of flow dynamics inside wall cavity and strut cavity placed in supersonic airflows von Dhankarghare, A. A., Jayachandran, T., Muruganandam, T. M.

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Active Control of Lean Blowout for Turbine Engine Combustors von Muruganandam, T. M, Nair, S, Scarborough, D, Neumeier, Y, Jagoda, J, Lieuwen, T, Seitzman, J, Zinn, B

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Investigation of Soot in a Model CFM56 Atmospheric Combustor Using In-Situ Laser-Induced Incandescence Calibration von Krishnasamy Bharathi, Arvind, Shrivastava, Poorva, Srivatsav, Hrishikesh, T. M., Muruganandam, K., Vasudevarao

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Affordable schlieren visualization methods for understanding three-dimensional supersonic flows von Vaisakh, S., Muruganandam, T. M.

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Optical equivalence ratio sensors for gas turbine combustors von Muruganandam, T.M., Kim, B.-H., Morrell, M.R., Nori, V., Patel, M., Romig, B.W., Seitzman, J.M.

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Effect of duct aspect ratio on normal shock wave/boundary layer interaction von Vaisakh, S., Namratha, P. R., Muruganandam, T. M.

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The 2.5 s Microgravity Drop Tower at National Centre for Combustion Research and Development (NCCRD), Indian Institute of Technology Madras von V.V., Nikhil, Nair, Abhilash, P, Niketh, Kumar, Amit, T.M., Muruganandam

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Modeling of destructive interaction of hot jet and solid plate von Muruganandam, T M, Son, E E, Gadzhiev, M Kh, Vetchinin, S P

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