... of the vane pressure field and the rotor pressure field create moving regions of high pressure and low pressure at the exit of the cavity. This results in pulsing regions of injection and ingestion. 17 08 2010 23 08 2010 15 07 2011 15 07 2011 aerospace components blades coolants...

... known as boundary-layer-ingesting (BLI) inlet. aerospace components aircraft boundary layer turbulence flow control Navier-Stokes equations transonic flow 06 07 2010 02 08 2010 15 07 2011 15 07 2011 Representative B-spline patch used to parameterize...

... engines, and possibly as much as 7% in smaller engines operating at higher altitudes ( 4 5 ). Prediction and control of suction side separation, without sacrifice of the benefits of higher loading, are, therefore, crucial for improved engine design. aerodynamics aerospace components boundary...

... 2008 22 02 2009 19 04 2011 19 04 2011 aerodynamics aerospace components bubbles coatings compressors computational fluid dynamics gas turbines Mach number Navier-Stokes equations turbulence Transonic or supersonic compressor blades typically have leading edge...

..., as shown in Table 1 , which represents the average value and the variation over the experiments that comprise this investigation. 22 07 2009 26 07 2009 11 11 2010 11 11 2010 aerodynamics aerospace components blades distortion high-pressure effects rotors turbines turbo...

... nonequilibrium thermodynamics multiphase flow interphase slip surface film droplet spectrum droplet splashing airfoil flow-angle deviation aerodynamics aerospace components aerospace engines aircraft blades calibration compressors evaporation gas turbines mass transfer nozzles 19 10...

... component volume dynamics modeling of a turbojet engine that will be used for an integrated vehicle aeropropulsoservoelastic model and for propulsion efficiency studies. 30 06 2008 04 02 2009 26 04 2010 26 04 2010 aerospace components aerospace propulsion aircraft compressors...

... ,” ASME J. Heat Transfer 0022-1481 , 103 , pp. 337 – 342 . 10.1115/1.3244463 aerospace components aerospace engines aircraft blades cooling gas turbines infrared imaging nozzles In recent years, the operating temperatures of gas turbines have continuously increased...

... the wake passing. As before the lines with white symbols represent the losses with unsteady inflow. KSI for steady and unsteady conditions, i = 0 / + 7   deg , Ra = 5   μ m 11 09 2008 15 02 2009 05 04 2010 05 04 2010 aerospace components...

.... , 1969 , “ Discharge Coefficients for Thick Plate Orifices With Approach Flow Perpendicular and Inclined to the Orifice Axis ,” NASA Technical Report No. TN D-5467. 26 08 2008 01 03 2009 05 04 2010 05 04 2010 aerospace components aircraft design engineering durability...

... to 100,000. 19 08 2008 27 02 2009 02 04 2010 02 04 2010 aerospace components aerospace engines approximation theory channel flow convection cooling design engineering gas turbines hydraulic systems turbulence Gas turbine engines are used in many applications...

.... This lack of commercial use is the motivation for the current study. gas turbine tandem blade compressor rotor computational aerospace components aerospace engines blades compressors gas turbines numerical analysis rotors 29 09 2008 28 01 2009 25 03 2010 25 03...

... minus the 2D loss. This loss breakdown is compared with the result for the “rest” loss ζ rest in correlation 10 ( 40 ) in Fig. 7 . aerospace components aerospace engines design engineering Mach number optimisation turbines The weight and cost of a low pressure turbine...

... and in optimizing the overall temperature distribution of the blade. 14 07 2008 09 03 2009 24 03 2010 24 03 2010 aerospace components aerospace engines aerospace industry blades bubbles cooling flow separation flow simulation lightweight structures liquid films Navier...

... of airfoils. Since the flow is subsonic, wakes from the upstream blade rows, which periodically pass through a downstream blade row, provide the dominant source of unsteadiness in the LP turbine. In this case, the wakes can reduce the size of separation. aerospace components boundary layer turbulence...

... and potentially open the design envelope. aerodynamics aerospace components blades flow visualisation pressure measurement turbines velocity measurement 2010 American Society of Mechanical Engineers ...

... could be as large as 7% in smaller engines operating at higher altitudes ( 4 5 ). Prediction and control of suction side separation, without sacrifice of the benefits of higher loading, are therefore crucial for improved engine design. aerodynamics aerospace components anemometry boundary...

... 2008 06 07 2009 aerodynamics aerospace components blades boundary layer turbulence bubbles compressors computational fluid dynamics flow measurement flow separation laminar flow pressure measurement stators wakes 2007 IGTI Best Technical Paper The leading-edge...

... of RSM, enhancement of existing EVM presents an important practical alternative. aerospace components confined flow rotational flow turbomachinery turbulence 2009 American Society of Mechanical Engineers ...

... experiencing thermal and mechanical fatigue, which can be better managed if the true turbine inlet conditions are well known and understood. aerospace components aerospace engines aerospace propulsion blades combustion combustion equipment convection gas turbines 26 07 2007 05 12...