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Keywords: pressure control
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Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2003, 125(3): 497–504.
Published Online: August 27, 2003
... aircraft boundary layer turbulence pressure control vortices rotors Few successful attempts have been made to reduce secondary loss through application of end-wall profiling to a blade row. One successful application of profiling has been demonstrated in the Linear Cascade at Durham University...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2003, 125(1): 128–132.
Published Online: January 23, 2003
... into the gas turbines higher output, efficiency, and lower heat rate. It is the achievement of this goal that has led us to develop an improved design for the GE frame engine gas turbine exhaust system. gas turbine power stations heat transfer pressure control flow separation flow control...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2002, 124(3): 393–401.
Published Online: July 10, 2002
... 10 07 2002 gas turbines aircraft boundary layer turbulence shear turbulence pressure control wakes flow separation The intense competition within the airline industry creates sustained pressure to achieve reductions in both the cost of manufacture and the weight of modern...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2002, 124(3): 402–409.
Published Online: July 10, 2002
.... gas turbines aircraft flow separation pressure control surface phenomena 04 June 2001 20 October 2000 10 07 2002 Contributed by the International Gas Turbine Institute and presented at the International Gas Turbine and Aeroengine Congress and Exhibition, New Orleans...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. October 2001, 123(4): 815–822.
Published Online: February 1, 2001
... 2001 01 February 2001 engines aerodynamics jets seals (stoppers) heat transfer pressure control leak detection finite element analysis temperature measurement gas turbines Labyrinth seals represent an important flow element in the secondary air system of aero engines...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2001, 123(1): 133–139.
Published Online: February 1, 2000
... February 2000. Paper No. 2000-GT-232. Review Chair: D. Ballal. 08 May 2000 01 February 2000 gas turbines heat transfer channel flow cooling pressure control The desire for increased gas turbine reliability and efficiency has spurred research in all areas of turbine blade...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2001, 123(1): 9–13.
Published Online: February 1, 2000
... 2000 gas turbines flow control aircraft 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...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2001, 123(1): 64–72.
Published Online: February 1, 2000
... received by the International Gas Turbine Institute February 2000. Paper No. 2000-GT-461. Review Chair: D. Ballal. 08 May 2000 01 February 2000 centrifuges rotational flow rough surfaces boundary layers shear flow flow separation pressure control Centrifugal Blower Vaneless...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2001, 123(2): 189–197.
Published Online: February 1, 2000
... altitude. Accurate prediction of separation and reattachment is, therefore, crucial to improved turbine design. gas turbines boundary layer turbulence velocity measurement laminar to turbulent transitions bubbles pressure control flow separation 08 May 2000 01 February 2000...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2001, 123(2): 296–304.
Published Online: February 1, 2000
... received by the International Gas Turbine Institute February 2000. Paper No. 2000-GT-476. Review Chair: D. Ballal. 08 May 2000 01 February 2000 gas turbines rotors pressure control vortices laser Doppler anemometry loss measurement The effects of the clearance flow have...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. October 2000, 122(4): 717–724.
Published Online: February 1, 2000
... airfoil design. Reliable experimental data are also important to develop and validate computational codes to predict blade metal temperatures, and an efficient cooling system design. gas turbines heat transfer pressure control rotors flow measurement 08 May 2000 01 February 2000...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2001, 123(2): 258–265.
Published Online: February 1, 2000
... Chair: D. Ballal. 08 May 2000 01 February 2000 gas turbines cooling film flow nozzles pressure control Mach number engines The rotor and nozzle guide vane (NGV) stages of the high-pressure turbine often incorporate discrete hole film cooling in an attempt to “insulate...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2000, 122(3): 494–504.
Published Online: February 1, 1999
..., 1999. Manuscript received by the International Gas Turbine Institute February 1999. Paper No. 99-GT-433. Review Chair: D. C. Wisler. 07 June 1999 01 February 1999 subsonic flow pressure control losses calibration boundary layers flow separation Despite the progress...
Journal Articles