Relevant bibliographies by topics / Engine icing

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Engine icing'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Engine icing"

1

Bartlett, C. S. "Turbine Engine Icing Spray Bar Design Issues." Journal of Engineering for Gas Turbines and Power 117, no. 3 (1995): 406–12. http://dx.doi.org/10.1115/1.2814110.

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Techniques have been developed at the Engine Test Facility (ETF) of the Arnold Engineering Development Center (AEDC) to simulate flight through atmospheric icing conditions of supercooled liquid water droplets. Ice formed on aircraft and propulsion system surfaces during flight through icing conditions can, even in small amounts, be extremely hazardous. The effects of ice are dependent on many variables and are still unpredictable. Often, experiments are conducted to determine the characteristics of the aircraft and its propulsion system in an icing environment. Facilities at the ETF provide t
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2

Yamazaki, Masafumi, Aleksandar Jemcov, and Hirotaka Sakaue. "A Review on the Current Status of Icing Physics and Mitigation in Aviation." Aerospace 8, no. 7 (2021): 188. http://dx.doi.org/10.3390/aerospace8070188.

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Icing on an aircraft is the cause of numerous adverse effects on aerodynamic performance. Although the issue was recognized in the 1920s, the icing problem is still an area of ongoing research due to the complexity of the icing phenomena. This review article aims to summarize current research on aircraft icing in two fundamental topics: icing physics and icing mitigation techniques. The icing physics focuses on fixed wings, rotors, and engines severely impacted by icing. The study of engine icing has recently become focused on ice-crystal icing. Icing mitigation techniques reviewed are based o
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MA, HUI, WEIJIAN CHEN, and DALIN ZHANG. "NUMERICAL INVESTIGATION OF ENGINE INLET VANE HOT–AIR ANTI–ICING SYSTEM WITH SURFACE AIR FILM." International Journal of Modern Physics: Conference Series 19 (January 2012): 331–40. http://dx.doi.org/10.1142/s2010194512008926.

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The inlet vane of aircraft engine needs to be equipped with anti-icing system to prevent ice accretion on the leading edge due to flight safety requirements, and the engine bleed hot-air is mostly used to heat the vane surface in anti-icing system. In order to save the energy consumption, a new anti-icing structure was developed and investigated with numerical simulation. Besides the use of small tunnels to enhance the heat transfer characteristics, a narrow gap was opened and assigned on the vane surface at the end of the anti-icing tunnels, and the exhaust hot-air was released from the gap t
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Dong, W., J. Zhu, M. Zheng, G. L. Lei, and Z. X. Zhou. "Experimental Study on Icing and Anti-Icing Characteristics of Engine Inlet Guide Vanes." Journal of Propulsion and Power 31, no. 5 (2015): 1330–37. http://dx.doi.org/10.2514/1.b35679.

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Gębura, Andrzej, Kazimierz Janusiak, and Michał Poradowski. "An Icing Of Aircraft – Reasons, Consequences, Counteraction." Journal of KONBiN 32, no. 1 (2014): 57–70. http://dx.doi.org/10.2478/jok-2014-0031.

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Abstract The article presents reasons of an helicopter’s ising as well as an aircraft’s ising. The maion attention is addressed a conteraction of an ising. Autors divide the problem an two groups: an ising of an airframe – mostly lifting surfaces, an ising of engines. According to authors reasons, an extension (first of all) consequences of airframe’s ising considerably differ from seemingly similar events in an engine. The considerable attention is concentrated on a connteraction of consequences of an ising during the flight. The most complicated ising referes to helicopters, considering thei
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Jérôme, Emilie, Franck Hervy, and Séverine Maguis. "Icing test capabilities at DGA Aero-engine Testing." International Journal of Engineering Systems Modelling and Simulation 8, no. 2 (2016): 77. http://dx.doi.org/10.1504/ijesms.2016.075562.

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Al-Khalil, Kamel M., Theo G. Keith, Kenneth J. DeWitt, James K. Nathman, and Donald A. Dietrich. "Thermal analysis of engine inlet anti-icing systems." Journal of Propulsion and Power 6, no. 5 (1990): 628–34. http://dx.doi.org/10.2514/3.23264.

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HAYASHI, Ryosuke, and Makoto YAMAMOTO. "Modelling of ice shedding phenomenon for engine fan icing." Transactions of the JSME (in Japanese) 80, no. 815 (2014): CM0209. http://dx.doi.org/10.1299/transjsme.2014cm0209.

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Haggerty, Julie, Eric Defer, Adrianus De Laat, et al. "Detecting Clouds Associated with Jet Engine Ice Crystal Icing." Bulletin of the American Meteorological Society 100, no. 1 (2019): 31–40. http://dx.doi.org/10.1175/bams-d-17-0252.1.

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AbstractIn the past two decades, more than 150 jet engine power-loss and damage events have been attributed to a phenomenon known as ice crystal icing (ICI). Ingestion of large numbers of ice particles into the engine core are thought to be responsible for these events, which typically occur at high altitudes near large convective systems in tropical air masses. In recent years, scientists, engineers, aviation regulators, and airlines from around the world have collaborated to better understand the relevant meteorological processes associated with ICI events, solve critical engineering problem
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Simpson, M. P., and P. M. Render. "Investigation of the certification and operational procedures for turboprop aircraft in icing." Aeronautical Journal 103, no. 1028 (1999): 449–54. http://dx.doi.org/10.1017/s0001924000064393.

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Abstract A study was conducted to identify possible improvements to the current certification and operational procedures for turboprop powered aircraft operating in icing conditions. Information was gathered through a series of interviews with airframe and engine manufacturers and also, operators and aircrews in Europe and Canada. The significant issues raised during the interviews are discussed, and a number of recommendations are made for future research and development activities in die area of aircraft icing. These recommendations identify the need for improved ice protection methods, enha
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Dissertations / Theses on the topic "Engine icing"

1

Horoufi, Aryan. "Car engine breather icing." Thesis, Cranfield University, 2012. http://dspace.lib.cranfield.ac.uk/handle/1826/10201.

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Icing in an engine breather system can block the engine breather pipe, cause excessive crankcase pressure and degrade the engine performance. In this project, a numerical study, experimental tests and CFD analysis are employed in order to understand condensation and the extent of freezing inside a vertical pipe, a horizontal pipe and a T-joint pipe which are exposed to an external convective cooling. The pipe internal flow is assumed to be a vapour/air mixture. This study has led an evaluation of freezing in an engine breather pipe. The finding in this project highlighted the effects of the pi
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Kundu, Reema. "Impact of engine icing on jet engine compressor flow dynamics." Diss., Georgia Institute of Technology, 2015. http://hdl.handle.net/1853/54870.

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Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This previously unrecognized form of icing occurs in flights through high altitude convective regions and vicinity of thunderstorms. Engine icing events involve power loss or damage associated to the engine core, namely instabilities such as compressor surge, stall, engine rollback and even combustor flameout events. The effects on compressor performance are significant in understanding the response of the engine to atmospheric ice ingestion. A one-dimensional axisymmetric flow model is used to simulate
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Ivey, P. C. "Self-induced flow in a rotating tube." Thesis, University of Sussex, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308072.

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Wade, S. J. "Modelling of the performance of a thermal anti-icing system for use on aero-engine intakes." Thesis, Loughborough University, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.376071.

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Riley, S. J. "Investigations relating to factors influencing the effectiveness of an aero-engine intake thermal anti-icing system." Thesis, Loughborough University, 1991. https://dspace.lboro.ac.uk/2134/7201.

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Thermal anti-icing systems are commonly used to protect aircraft leading edges from a potentially hazardous build-up of ice. Such systems have proven reliable in service and are relatively cheap and efficient. Typically, hot air is tapped from the engine compressor and ducted (via a regulation and control system) to the surface to be protected. Ideally an optimisation process should be employed at the design stage in order to ensure adequate anti-icing capability with minimal use of engine bleed air, since the latter represents a performance penalty. Following submission by the author of an MS
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Oliver, Michael James. "A STUDY ON THE PHYSICS OF ICE ACCRETION IN A TURBOFAN ENGINE ENVIRONMENT." Case Western Reserve University School of Graduate Studies / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=case1363875844.

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Valíček, Jan. "Statické a dynamické posouzení konstrukce vyhlídkové věže." Master's thesis, Vysoké učení technické v Brně. Fakulta stavební, 2013. http://www.nusl.cz/ntk/nusl-226476.

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This thesis deals with static and dynamic analysis of an lookout tower construction. For dynamic analysis a computational model in ANSYS software is created. Static analysis is performed by Scia Engineer software. Both of this software use finite element method. It is also focused on wind load determination by Eurocode 1, structural factor calculation, modal analysis and vortex shedding. Verification of selected parts according to Eurocodes is included.
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Hutchings, Rick. "Effects of Supercooled Water Ingestion on Engine Performance." 2011. http://trace.tennessee.edu/utk_gradthes/981.

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An aircraft will encounter freezing rain, snow, and ice during ground operation and flight. In cold conditions, ice may form on th einlet and internal stators and rotors of the gas turbine engine. When ice accumulates on blades (and/or stators), the aerodynamic characteristics of the blades change due to the altered size, shape, and roughness. This change causes the blade to no longer operate at its design point and decreases compressor performance. Therefore, characterization of the aerodynamic performance is required to define the associated losses due to the effects of supercooled liqui
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Books on the topic "Engine icing"

1

Piston engine icing. Civil Aviation Authority, 1991.

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2

Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet. National Aeronautics and Space Administration, 1995.

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R, Mohler Stanley, and United States. National Aeronautics and Space Administration., eds. Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet. National Aeronautics and Space Administration, 1995.

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4

Wade, S. J. Modelling of the performance of a thermal anti-icing system for use on aero-engine intakes. 1986.

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5

Riley, S. J. Investigations relating to factors influencing the effectiveness of an aero-engine intake thermal anti-icing system. 1991.

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6

An experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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7

Snider, Jill D. Lucean Arthur Headen. University of North Carolina Press, 2020. http://dx.doi.org/10.5149/northcarolina/9781469654355.001.0001.

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Born in Carthage, North Carolina, Lucean Arthur Headen (1879-1957) grew up amid former slave artisans. Inspired by his grandfather, a wheelwright, and great-uncle, a toolmaker, he dreamed as a child of becoming an inventor. His ambitions suffered the menace of Jim Crow and the reality of a new inventive landscape in which investment was shifting from lone inventors to the new “industrial scientists.” But determined and ambitious, Headen left the South, and after toiling for a decade as a Pullman porter, risked everything to pursue his dream. He eventually earned eleven patents, most for innova
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Book chapters on the topic "Engine icing"

1

Iwago, Mikiko, Koji Fukudome, Hiroya Mamori, Naoya Fukushima, and Makoto Yamamoto. "Fundamental Investigation to Predict Ice Crystal Icing in Jet Engine." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-1892-8_25.

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Snider, Jill D. "Epilogue." In Lucean Arthur Headen. University of North Carolina Press, 2020. http://dx.doi.org/10.5149/northcarolina/9781469654355.003.0011.

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The epilogue reflects on what invention meant to Headen and to the larger artisanal class from which he came and examines his legacy. Addressed are his influence on other African American transportation technology pioneers, his encouragement of mechanization among British farmers, the role of his bi-fuel engine improvements in supporting the British war effort in World War II, and his long-term influence on engine designs and on anti-icing technologies for air and rotor craft, turbine engines, and wind turbines. The epilogue also probes historiographical questions illuminated by Headen’s story, including the nature of African American automobility in the 1920s, specifically the participation of black beauty culturalists as investors and the automobile’s role in expanding African American social networks; the influence of early religious leaders on the business strategies of African American entrepreneurs; and the implications that social networks carry for personal success and for future racial advancement.
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Snider, Jill D. "Introduction." In Lucean Arthur Headen. University of North Carolina Press, 2020. http://dx.doi.org/10.5149/northcarolina/9781469654355.003.0001.

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The Introduction provides an overview of the life of early African American inventor, aviator, auto racer, engineer, and entrepreneur, Lucean Arthur Headen, It also prefaces the biography’s main themes, including Headen’s childhood influences; the obstacles he faced as an African American independent inventor, including segregation and the increasing corporatization of invention; the social networks on which he relied to build his career; the “coalition economics” strategy he employed to succeed; his emigration to England in 1931 and his career there until his death in 1957; his legacy as a designer of automotive engine improvements and anti-icing methods for aircraft; and his role as a transportation technology promoter.
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Snider, Jill D. "A Dream Crosses the Pond." In Lucean Arthur Headen. University of North Carolina Press, 2020. http://dx.doi.org/10.5149/northcarolina/9781469654355.003.0010.

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Chapter 9 discusses Headen’s professional and personal life between his emigration to England in 1931 until his death there in 1957. It documents the companies he directed in Camberley, Surrey, principally Headen Hamilton Engineering Co., Ltd. (with investor George D. Hamilton) and Headen Keil Engineering Co., Ltd. (with local builder James Richard McLean Keil), and the companies that distributed the bi-fuel engine kits he patented and manufactured for automobiles, lorries, and Fordson tractors. Addressing his legacy as an inventor, the chapter also explores the contributions his products made to British agriculture in the 1930s and to the war effort in World War II, and the long-reaching impact of anti-icing methods he patented for aircraft. Finally, the chapter examines Headen’s social position in England; his service in the Surrey Home Guard; his remarriage in 1945; his adoption of a son in 1948; and his death in Frimley Green in 1957.
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Conference papers on the topic "Engine icing"

1

Hirvonen, J., K. Säntti, S. Niemelä, R. Hyvönen, K. Ahti, and K. E. J. Lehtinen. "An Icing Index Comparison to Luosto Icing Measurements." In 2007 SAE Aircraft and Engine Icing International Conference. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3305.

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Venkataramani, K., R. Plybon, Raymond Holm, and Brian Krupp. "Aircraft Engine Icing Model." In 46th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-440.

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Dyer, Kirsten P. "Anti-Icing Fluid Residues." In 2007 SAE Aircraft and Engine Icing International Conference. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3302.

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Bidwell, Colin. "Icing Analysis of the NASA S3 Icing Research Aircraft Using LEWICE3D Version 2." In 2007 SAE Aircraft and Engine Icing International Conference. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3324.

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Bartlett, C. Scott. "Turbine Engine Icing Spray Bar Design Issues." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-340.

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Techniques have been developed at the Engine Test Facility (ETF) of the Arnold Engineering Development Center (AEOC) to simulate flight through atmospheric icing conditions of supercooled liquid water droplets. Ice formed on aircraft and propulsion system surfaces during flight through icing conditions can, even in small amounts, be extremely hazardous. The effects of ice are dependent on many variables and are still unpredictable. Often, experiments are conducted to determine the characteristics of the aircraft and its propulsion system in an icing environment. Facilities at the ETF provide t
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6

Zeppetelli, Danial, and Wagdi G. Habashi. "CFD-Icing: A Predictive Tool for In-Flight Icing Risk Management." In SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing. SAE International, 2011. http://dx.doi.org/10.4271/2011-38-0031.

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Mazzawy, Robert S., and J. Walter Strapp. "Appendix D - An Interim Icing Envelope." In 2007 SAE Aircraft and Engine Icing International Conference. SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3311.

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Mingione, Giuseppe, Emiliano Iuliano, Didier Guffond, and Cameron Tropea. "EXTICE: EXTreme Icing Environement." In SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing. SAE International, 2011. http://dx.doi.org/10.4271/2011-38-0063.

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Serke, David, John Hubbert, Andrew Reehorst, et al. "In-flight Icing Hazard Verification with NASA's Icing Remote Sensing System for Development of a NEXRAD Icing Hazard Level Algorithm." In SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing. SAE International, 2011. http://dx.doi.org/10.4271/2011-38-0030.

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Reinert, Tonja, Robert J. Flemming, Robert Narducci, and Roger J. Aubert. "Oscillating Airfoil Icing Tests in the NASA Glenn Research Center Icing Research Tunnel." In SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing. SAE International, 2011. http://dx.doi.org/10.4271/2011-38-0016.

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