Items where Author is "Mohan, K"

Mohan, K and Guruprasad, SA (1994) Effect of axially non-uniform rotor tip clearance on the performance of a high speed axial flow compressor stage. In: ASME, International Gas Turbine and Aeroengine Congress and Exposition, 13-16 June 1994, Hague, Netherlands.

Guruprasad, SA and Mohan, K (1991) Novel technique for the experimental determination of bearing and windage losses in an axial flow compressor. In: 10th International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.

Nagapurwala, QH and Girigoswamy, H and Mohan, K (1987) Effect of variable geometry inlet guide vanes on the performance of a high speed compressor stage. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Mohan, K (1986) Design of an axial flow research compressor operating in the subsonic and transonic ranges. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Girigoswami, H and Mohan, K (1986) Novel loading device for testing high power drive systems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mohan, K and Nagpurwala, QH and Girigoswamy, 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.