Items where Author is "Nagpurwala, QH"

Up a level
Export as [feed] RSS 2.0 [feed] RSS 1.0 [feed] Atom
Group by: Item Type | No Grouping
Number of items: 12.

Kumaran, S and Kamble, S and Swamy, KMM and Nagpurwala, QH and Bhat, A (2015) Effect of Axial Velocity Density Ratio on the Performance of a Controlled Diffusion Airfoil Compressor Cascade. International Journal of Turbo and Jet Engines . pp. 1-13. ISSN 2191-0332

Prathapanayaka, R and Nagpurwala, QH and Shembharkar, TR (2006) Analytical Design and Evaluation of a Controlled Diffusion Aerofoil Blade for a LP Compressor Stator. Technical Report. NAL, Bangalore.

Nagpurwala, QH and Shobhavathy, MT (2002) Some Experimental Studies on Airjet and Solid Body Vortex Generators. In: Proceedings of the Ninth Asian Congress of Fluid Mechanics.

Nagpurwala, QH and Guruprasad, SA and Girigoswami, H and Pai, BR (1995) Experimental and analytical studies of a transonic stator having controlled diffusion aerofoil with end bends. In: 12th ISABE - International Symposium on Air Breathing Engines, 10-15 Sept 1995, Melbourne, Australia.

Nagpurwala, QH (1989) Software modules for analysing and plotting the probe calibration data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH and Rammohan, K (1989) Development of a software package for automatic data acquisition, analysis, and controls in an axial flow compressor test rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH (1988) Recovery characteristics of three shielded thermocouple13; temperature probes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH (1987) Non-nulling calibration of a two-dimensional combination wedge probe. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH (1987) Design and calibration of three hole cylinderical13; combination probes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH (1986) Pressure velocity flow direction and mass flow measurements in cascade and turbomachinery testing. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mohan, K and Nagpurwala, QH and Girigoswami, H and Guruprasad, SA (1981) High speed axial flow compressor research facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Nagpurwala, QH and Mohan, K (1974) Proposed instrumentation for compressor research rig. Technical Report. National Aeronautical Laboratory, Bangalore, India.

This list was generated on Tue Sep 27 02:33:12 2016 IST.