Nonlinear Characteristics of a Rectangular Cavity in Supersonic Flow von Pandian, S, Desikan, S. L. N, Niranjan, Sahoo

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Supersonic Combustion of a Scramjet Engine Using Hydrogen Fuel in Shock Tunnel von Srinivasan, K, Maurya, Praveen K, Abhishek, Kumar, Desikan, S. L. N, Murugan, B

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Onset of Transient Shock Interaction with Cavity Shear Layer von Pandian, S, Desikan, S. L. N, Niranjan, Sahoo

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Longitudinal Aerodynamics of a Winged Reentry Vehicle at Supersonic Speed von Desikan, S. L. N, Srinivasan, K

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Unsteadiness in vacuum ejector and their sources von Raju, Martin, Desikan, S. L. N., Vaidyanathan, Aravind

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Transient characteristics of a typical vacuum ejector—An experimental study von Raju, Martin, Desikan, S. L. N., Vaidyanathan, Aravind

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Experiments on atomization and spray characteristics of an effervescent strut injector von Chakraborty, Mayukhmali, Vaidyanathan, Aravind, Desikan, S. L. N.

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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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Experimental investigation of starting characteristics and wave propagation from a shallow open cavity and its acoustic emission at supersonic speed von Pandian, S., Desikan, S. L. N., Niranjan, Sahoo

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Twin Jet Interaction and Reverse Flow von Desikan, S. L. N, Murugan, B, Srinivasan, K, Sajan, S

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Effect of Freestream–Plume Interaction on Launch Vehicle Aerodynamics von Desikan, S. L. N, Suresh, K, Saravanan, R, Patil, M. M, Balasubramanian, P, Prasath, M

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Onset of Cavity Oscillation From Transverse to Longitudinal Mode in a Supersonic Flow von Pandian, S, Desikan, S. L. N, Niranjan, Sahoo

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Effect of Leading-Edge Bluntness on Shockwave–Boundary-Layer Interaction in a Scramjet Intake von Vamsi Krishna, Talluri, Sreekumar, Jithin, Ibrahim Sugarno, Mohammed, Desikan, S. L. N.

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Effect of Cold Jet Plume on Aerodynamics Coefficients von Desikan, S. L. N, Saravanan, R, Suresh, K, Tennyson, J. A, Chandrasekar, N, Subramanian, S, Patil, M. M

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Effect of cavity rear wall modifications on pressure fluctuations at supersonic speed von Krishna, T.V., Kumar, P., Das, S., Desikan, S.L.N.

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Effect of back pressure and freestream dynamic pressure on a typical Ramjet engine duct under realistic supersonic inlet condition von Saravanan, R., Desikan, S.L.N., Muruganandam, T.M.

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Investigation of Supersonic Jet Interaction With Hypersonic Cross Flow von Desikan, S. L. N, Saravanan, R, Subramanian, S, Sivararamakrishnan, A. E, Pandian, S

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Strut-Based Gaseous Injection into a Supersonic Stream von Desikan, S. L. N, Kurian, Job

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Experimental investigation of start/unstart process during hypersonic intake at Mach 6 and its control von Saravanan, R., Desikan, S.L.N., Francise, K.J., Kalimuthu, R.

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Experiments on flow past cavity and the application of modal decomposition techniques von Desikan, S.L.N., Pandian, S., Simha, Padmanabha Prasanna, Sahoo, Niranjan

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