... an appropriate value of initial tangential velocity. gas turbines cooling flow simulation combustion temperature control flow measurement compressors rotational flow The internal air system of a modern gas turbine provides air to cool and seal various components around the engine. Such air...

... Institute February 2000. Paper No. 2000-GT-33. Review Chair: D. Ballal. 08 May 2000 01 February 2000 compressors gas turbines stators aerodynamics fault diagnosis temperature control geometry Incorporating variable geometry into the stages of axial compressors...

... flow temperature control evaporation To improve the overall efficiency of gas turbine engines, the turbine inlet temperature and compressor pressure ratio are continuously increasing for the next generation of gas turbine systems. As a result, even with the potential advancement of future...

... engines temperature control pressure control compressors Rotating stall and surge are two undesirable instabilities in gas turbine engines. Either instability can be initiated by poor inlet flow conditions in the engine. Nonuniform inlet conditions (known as distorted inlet conditions) can...

... and Aeroengine Congress and Exposition, Orlando, Florida, June 2–5, 1997. Manuscript received at ASME Headquarters February 1997. Paper No. 97-GT-255. Associate Editor: H. A. Kidd. 02 June 1997 01 February 1997 gas turbines wakes cooling film flow jets temperature control...