Publications
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. Computational Investigation of Effect of Axial Spacing on Blade Row Interaction in a 1½ Stage Axial Flow Turbine. Engineering Applications of Computational Fluid Mechanics. 2008.
. Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor. International Journal of Turbo and Jet Engines. 2008;24:195-205.
. Flow Measurements in Passages of Different Diffusers of a Centrifugal Compressor. Journal of Aerospace Sciences and Technologies. 2008;60:26-38.
. Flow Measurements in Passages of Different Diffusers of a Centrifugal Compressor. Journal of Aerospace Sciences and Technologies. 2008;60:26-38.
. Computational Study of the Effect of Sweep on the Performance and Flow Field in an Axial Flow Compressor Rotor. Proceedings of the Institution of Engineers, Part A: Journal of Power and Energy. 2007;221:315-329.
. Investigations on low speed axial compressor with forward and backward sweep. Journal of Thermal Sciences. 2007;16:121-133.
. Performance improvement of a low aspect ratio axial flow compressor by means of turbulence generator. Journal of Aerospace Sciences and Technologies. 2007;59:21-32.
. Unsteady Flow Behind Forward Swept Axial Compressor Rotors. International Journal of Fluid Mechanics Research. 2007;34:332-351.
. Unsteady Flow Behind Forward Swept Axial Compressor Rotors. International Journal of Fluid Mechanics Research. 2007;34:332-351.
. Effect of Diffuser Vane Height on Diffuser Wall Static Pressure Distribution in a Centrifugal Compressor. Journal of Aerospace Sciences and Technologies. 2006;58:322-337.
. Effect of Diffuser Vane Height and Position on the Performance of a Centrifugal Compressor. Proceedings of the Institution of Engineers, Part A: Journal of Power and Energy. 2004;218:647-654.
. Performance and Static Pressure Distribution on the Diffuser Walls of a Centrifugal Compressor using Different Types of Diffusers. Proceedings of the Institution of Engineers, Part A: Journal of Power and Energy. 2004;217:547-558.
. Experimental Investigation of Tip Clearance Effects on Flow Field in an Annular Turbine Rotor Cascade. Indian Journal of Engineering Science and Material Science. 2002;9:424-431.
. Finite Volume Analysis of Inviscid Interaction for Two-Dimensional Transonic Axial Turbine Stage Using Multi-Block Hybrid Grids. International Journal of Turbo and Jet Engines. 2002;19:157-177.
. Large Angle Calibration of Five Hole Probes. Journal of the Aeronautical Society of India. 2002;54:265-272.
. Geometry Based Hyperbolic Grid Generation for Computational Fluid Dynamics. AIAA Journal. 2001;39:1631-1633.
. Loss Reduction by means of Three Dimensional Roughness Elements on the Suction Surface of a Linear Cascade. Journal of the Aeronautical Society of India. 2000;52:1-8.
. Review: Recent Investigations on Tip Clearance Flows in Centrifugal Compressors. International Journal of Turbo and Jet Engines. 2000;17:65-78.
. Loss Reduction by means of Two Dimensional Roughness Elements on the Suction Surface of a Linear Cascade. Flow, Turbulence and Combustion. 1999;62:227-248.
. A Method of Calibration of Seven Hole Pressure Probe for Measuring Highly Three Dimensional Flows”,. Measurement Science and Technology. 1998;9:468-476.
