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Keywords: aircraft
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Journal Articles
Journal Articles
Article Type: Review Articles
J. Eng. Gas Turbines Power. December 2020, 142(12): 120801.
Paper No: GTP-20-1184
Published Online: December 2, 2020
...Luca Menegozzo; Ernesto Benini The present paper focuses on the numerical modeling approaches adopted in boundary layer ingestion (BLI) studies. Three driving aircraft concepts have been identified, namely propulsive fuselage concept (PFC), rear engines concept (REC), and distributed fans concept...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. January 2012, 134(1): 011501.
Published Online: October 28, 2011
... and aircraft applications. The unsteady flow field that disturbs the flame consists not only of the incident transverse acoustic wave, but also longitudinal acoustic fluctuations and vortical fluctuations associated with underlying hydrodynamic instabilities of the base flow. We show that the acoustic...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. October 2011, 133(10): 101601.
Published Online: May 6, 2011
...Marvin Zaluski; Sylvain Létourneau; Jeff Bird; Chunsheng Yang The CF-18 (CF denotes Canadian Forces) aircraft is a complex system for which a variety of data are systematically being recorded: flight data from sensors, built-in test equipment data, and maintenance data. Without proper analytical...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. June 2011, 133(6): 062503.
Published Online: February 17, 2011
...Peter Gloeckner; Klaus Dullenkopf; Michael Flouros Operating conditions in high speed mainshaft ball bearings applied in new aircraft propulsion systems require enhanced bearing designs and materials. Rotational speeds, loads, demands on higher thrust capability, and reliability have increased...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. March 2011, 133(3): 032503.
Published Online: November 12, 2010
... the oil flow to the air/oil separator, however, due to the oil flow distribution the thermal effects may lead to high material temperatures and to malfunctions in the engine’s lube system. 18 02 2010 22 06 2010 12 11 2010 12 11 2010 aerospace engines aircraft computational...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. March 2011, 133(3): 031702.
Published Online: November 11, 2010
...Alexandros Terzis; Charilaos Kazakos; Nikolaos Papadopoulos; Anestis Kalfas; Pavlos K. Zachos; Pericles Pilidis The penetration of a jet of fluid into a traversal moving stream is a basic configuration of a wide range of engineering applications, such as film cooling and V/STOL aircrafts...
Journal Articles
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. July 2010, 132(7): 072502.
Published Online: April 14, 2010
...Michael P. Enright; Kwai S. Chan; Jonathan P. Moody; Patrick J. Golden; Ramesh Chandra; Alan C. Pentz Fretting fatigue is a random process that continues to be a major source of damage associated with the failure of aircraft gas turbine engine components. Fretting fatigue is dominated...
Journal Articles
Journal Articles
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. April 2010, 132(4): 041604.
Published Online: January 27, 2010
... , “ Decision Support for Remote Monitoring and Diagnostics of Aircraft Engine Using Influence Diagrams ,” ASME Paper No. GT2007-28331. McDonald , R. A. , 2006 , “ The Mean Subjective Utility Score, a Novel Metric for Cost-Sensitive Classifier Evaluation ,” Pattern Recogn. Lett. 0167-8655 , 27...
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. January 2009, 131(1): 011201.
Published Online: November 20, 2008
...M. Kelaidis; N. Aretakis; A. Tsalavoutas; K. Mathioudakis An aircraft mission analysis procedure, accounting for engine aging deterioration and incorporating emission estimation capability, is presented. It consists of three main modules: a flight simulation module, an engine performance simulation...
Journal Articles
Journal Articles
Article Type: Research Papers
J. Eng. Gas Turbines Power. July 2008, 130(4): 042505.
Published Online: April 29, 2008
...-friction effects from the lubricant film and surfaces in contact, respectively. The test damper reproduces an aircraft application that must contain the lubricant for extended periods of time. The test damper journal is 2.54 cm in length and 12.7 cm in diameter, with a nominal clearance of 0.127 mm...
Journal Articles
Journal Articles
Article Type: Technical Papers
J. Eng. Gas Turbines Power. January 2006, 128(1): 1–7.
Published Online: October 21, 2004
...Jorge R. Camacho; Ahsan R. Choudhuri Buoyant and nonbuoyant shapes of methane flames issued from a 2:1 aspect ratio elliptic tube burner were measured. Nonbuoyant conditions were obtained in the KC-135 microgravity research aircraft operated by NASA’s Johnson Space Center. A mathematical model...
Journal Articles
Article Type: Technical Papers
J. Eng. Gas Turbines Power. July 2004, 126(3): 472–474.
Published Online: August 11, 2004
... aircraft gas turbines engines multivariable control systems Multivariable Controls (MVC’s) have been studied for use in aircraft gas turbine engines since the mid 1970s. The typical twin spool, afterburning turbofan engine used for most military applications exhibits coupling between a number...
Journal Articles
Article Type: Announcements And Other Notes
J. Eng. Gas Turbines Power. April 2004, 126(2): 442.
Published Online: June 7, 2004
...Dilip R. Ballal 07 06 2004 biographies gas turbines combustion aerodynamics ignition heat transfer sprays aerospace engines aircraft flames Professor Arthur H. Lefebvre, an ASME Fellow and a member of IGTI’s Combustion and Fuels technical committee over three...
Journal Articles
Article Type: Technical Papers
J. Eng. Gas Turbines Power. January 2004, 126(1): 40–44.
Published Online: March 2, 2004
... to find those technologies representing the best compromise between performance improvement and technology risk. Finally, a practical demonstration of the method and accompanying results is given for a typical commercial aircraft engine technology selection problem. Contributed by the International...