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Keywords: jet engines
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2012, 134(4): 041003.
Published Online: July 19, 2011
... 01 2010 24 11 2010 19 07 2011 19 07 2011 cooling gas turbines jet engines thermodynamics The constant increase of the fuel price requires an optimization of the engine design tool in order to increase the efficiency and the power density of each component...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2012, 134(2): 021009.
Published Online: June 23, 2011
... for vane failures. 24 09 2010 29 10 2010 23 06 2011 23 06 2011 blades elasticity failure (mechanical) fans jet engines stators Advanced design composite fan stators at Honeywell have encountered high amplitude vibrations during development. Sanders ( 1 ) reported...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2012, 134(1): 011023.
Published Online: June 1, 2011
... ducts flow separation flow visualisation jet engines vortices wakes Advanced requirements on future turbofans lead to conventional engines with high-bypass-ratios and large fans. Therefore, the low pressure (LP) turbine driving the fan has to rotate at a lower speed but at a much higher...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2012, 134(1): 011002.
Published Online: May 24, 2011
.... The results suggest that advanced open rotor designs can possibly meet Stage 4 noise requirements. 08 07 2010 05 09 2010 24 05 2011 24 05 2011 aerospace propulsion aircraft computational fluid dynamics fans flow instability flow simulation jet engines rotors wakes...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2011, 133(2): 021016.
Published Online: October 22, 2010
... blades compressors jet engines nozzles rotors stators turbines vibrations turbines compressors wave reflections nonsynchronous blade vibrations forced blade vibrations turbomachinery noise high cycle fatigue rotating stall Turbomachines can be seriously damaged...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2010, 132(4): 041003.
Published Online: April 26, 2010
... elasticity jet engines vehicle dynamics In many aeropropulsion applications, a relatively low fidelity engine model (i.e., without volume dynamics), which includes speed and temperature dynamics with the appropriate component performance characteristics, is adequate to design control laws...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2010, 132(3): 031017.
Published Online: April 5, 2010
...Marcus Hüning Gas turbines and jet engines consist of a network of connected cavities beside the main gas path called the secondary air system. These cavities, which are often surrounded by stationary and high angular speed rotating walls are exposed to varying pressure and temperature levels...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2010, 132(3): 031007.
Published Online: March 25, 2010
.... drag fans flow simulation jet engines Mach number mass transfer nozzles numerical analysis rotors 1 An important consideration in the design of nacelles for commercial aircraft engines is the propulsion system drag at engine-out “windmill” conditions, where the fan rotor...
Journal Articles
Publisher: ASME
Article Type: Technical Briefs
J. Turbomach. October 2009, 131(4): 044501.
Published Online: June 30, 2009
... negligible compared with the primary variables such as the suction ratio and extraction angle.o 07 12 2007 31 08 2008 30 06 2009 blades boundary layers channel flow combustion computational fluid dynamics cooling gas turbines heat conduction jet engines thin film devices...
Journal Articles
Publisher: ASME
Article Type: Igti Scholar Lecture
J. Turbomach. July 2009, 131(3): 031101.
Published Online: April 20, 2009
... to in the research community. The case histories of two projects are given to illustrate the point: the development of the concept of “smart jet engines” and the Silent Aircraft Initiative. In addition to providing a capability to attack multidisciplinary problems, the way in which collaboration can enhance...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2009, 131(3): 031011.
Published Online: April 9, 2009
... offers promising benefits at transient operation, leading to an improvement potential for the overall engine performance. 19 12 2007 04 02 2008 09 04 2009 aircraft blades compressors jet engines rotors turbines One of the most challenging problems in gas turbine engine...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2008, 130(3): 031005.
Published Online: May 2, 2008
... of the cooler. 27 07 2006 03 04 2007 02 05 2008 blades computational fluid dynamics cooling geometry jet engines jets stereo image processing turbines velocimeters wind tunnels Film cooling of gas turbine stator and rotor airfoil surfaces has played a major role...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2008, 130(2): 021002.
Published Online: February 12, 2008
.... , and Steele , W. G. , 1989 , Experimentation and Uncertainty Analysis for Engineers , Wiley , New York , pp. 47 – 131 . 13 08 2006 07 04 2007 12 02 2008 blades cooling gas turbines jet engines Mach number subsonic flow gas turbine blade tip film cooling...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2008, 130(1): 011007.
Published Online: December 19, 2007
.... , 1976 , “ Characterization of Components Performance and Optimization of Matching in Jet-Engine Development ,” AGARD-LS-83, pp. 7.1 – 7.19 . Riegler , C. , Bauer , M. , and Schulte , H. , 2003 , “ Validation of a Mixed Flow Turbofan Performance Model in the Sub-Idle Operating Range...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2007, 129(1): 119–126.
Published Online: January 1, 2007
... a series of accelerated deterioration tests on a General Electric J85-13 jet engine. The axial compressor was deteriorated by spraying atomized droplets of saltwater into the engine intake. The paper presents the overall engine performance deterioration as well as deteriorated stage characteristics...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2007, 129(1): 136–142.
Published Online: January 1, 2007
...Elisabet Syverud; Lars E. Bakken This paper reports the results of a series of online water wash tests of a GE J85-13 jet engine at the test facilities of the Royal Norwegian Air Force. The engine performance was deteriorated by injecting atomized saltwater at the engine inlet. The engine...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2007, 129(4): 669–678.
Published Online: December 21, 2006
... and calculations to demonstrate the behavior and gives guidance for the design of bleed slots by stressing the fundamental features of the flow. 07 12 2006 21 12 2006 jet engines compressors stators blades aerodynamics Bleed off-takes on the hub and casing endwalls, part way through...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2007, 129(4): 645–658.
Published Online: December 21, 2006
...B. A. Leishman; N. A. Cumpsty; J. D. Denton In a jet engine bleed off-takes on the hub and casing endwalls, part way through the compressor, supply high-pressure air for cooling, sealing, de-icing, and aircraft cabin air applications; bleed also assists compressor operation at part-speed conditions...