... of predictions of engine performance, efficiency, component life, gaseous emissions, and development and maintenance costs. calibration cooling engines heat conduction nozzles pressure measurement radiation stagnation flow temperature measurement thermocouples transducers valves 07 10...

... of inlet stagnation pressure profile for different amplitudes of inlet nonuniformity 20 07 2009 20 08 2009 21 10 2010 21 10 2010 blades compressors flow instability rotors stagnation flow transonic flow vortices wakes The design of highly loaded, high Mach...

... 2007 30 08 2007 29 01 2009 boundary layer turbulence heat transfer stagnation flow As engine manufacturers strive to raise turbine inlet air temperatures upwards to 3000 ° F ( 1650 ° C ) , they are limited by the life capability of the turbine airfoils...

.... 316 . 26 07 2007 03 01 2008 23 01 2009 blades combustion engines gas turbines stagnation flow turbulence The performance of gas turbine engines is highly dependent on the operation and durability of the hot section, which includes the combustor and high pressure...

... for predicting cascade stagnation-line heat transfer using only surface pressure calculations. aerodynamics boundary layers computational fluid dynamics flow simulation friction gas turbines laminar flow pressure measurement stagnation flow thermal resistance For example, consider the turbine...

... aerodynamics nozzles turbulence stagnation flow 09 03 2006 08 08 2006 2007 American Society of Mechanical Engineers ...

... streak itself. flow measurement boundary layer turbulence stagnation flow wakes heat transfer 13 June 2004 01 October 2003 01 March 2004 09 02 2005 Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS...

... June 2003 01 December 2002 01 March 2003 26 03 2004 heat transfer gas turbines turbulence aerodynamics nitrogen compounds computational fluid dynamics flow simulation stagnation flow nozzles heat exchangers Current approaches to achieving a low level of thermal...

... crystals laminar to turbulent transitions stagnation flow aerodynamics computational fluid dynamics gas turbines Turbine blade aerodynamics is generally given a high degree of analysis prior to commitment for fabrication. This attention to detail is carried through to the manufacturing...

...-GT-30520. Review Chair: E. Benvenuti. 03 June 2002 10 October 2001 23 04 2003 turbines aerodynamics cooling film flow flow simulation stagnation flow Navier-Stokes equations To achieve high cycle efficiency in modern gas turbine engines, the temperature...

...N. A. Cumpsty, Chief Technologist, compressors centrifuges optimisation fluid dynamics turbulence stagnation flow I found this an interesting and original paper. Although I do not pretend to understand the details of the optimization procedure, I am interested in the predictions...

... p and ω are comparable in their magnitudes between the original and the other cases. Therefore, the end configurations are less dependent on the coefficients used and very close to each other. compressors centrifuges fluid dynamics optimisation turbulence stagnation flow...

...N. A. Cumpsty [S0889-504X(00)01303-9] gas turbines measurement systems compressors probes flow control pressure sensors fluctuations stagnation flow This paper and its two companions (Parts 1&2) describe careful and meticulous work and I therefore hesitate to offer any...

... stagnation flow temperature measurement flow visualisation infrared spectra channel flow cooling To reduce or eliminate the need to employ film cooling, new attention has been devoted to internal cooling schemes for turbine airfoils. Internal schemes are advantageous in several respects...

.... Review Chair: D. Ballal. 08 May 2000 01 February 2000 gas turbines heat transfer stagnation flow combustion gas turbine power stations turbulence wind tunnels Firing temperatures of modern turbine engines often exceed the melting temperature of the downstream blade...

... and Aeroengine Congress and Exhibition, Munich, Germany, May 8–11, 2000. Manuscript received by the International Gas Turbine Institute February 2000. Paper No. 2000-GT-221. Review Chair: D. Ballal. 08 May 2000 01 February 2000 gas turbines cooling heat transfer jets steam stagnation...