Academic literature on the topic 'Aircraft icing'

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Journal articles on the topic "Aircraft icing"

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Yang, Qin Yu, Jin Bo Yao, Yue Ming Yang, and Xue Wei Liu. "In the Wind Tunnel Simulation Defroster Control Study." Applied Mechanics and Materials 380-384 (August 2013): 191–94. http://dx.doi.org/10.4028/www.scientific.net/amm.380-384.191.

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Aircraft in flight, such as supercooled water droplets encountered icing conditions suitable for the external environment, the relevant parts of the body will freeze, making the aircraft's aerodynamic performance deterioration, severe endanger flight safety, in addition, the aircraft parked in the open winter months , there will be icing, you need to clean up before takeoff. We should grasp the mechanism of aircraft icing, environmental factors and easy to freeze parts of the body. This paper presents a simulation using the wind tunnel icing device icing wind tunnel simulations can reproduce t
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Yao, Jin Bo, Yue Ming Yang, Qin Yu Yang, Xiu Juan Liu, and Dun Jin. "Application of LED Light Source in the Flow Imaging." Applied Mechanics and Materials 380-384 (August 2013): 219–22. http://dx.doi.org/10.4028/www.scientific.net/amm.380-384.219.

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Aircraft in flight, such as supercooled water droplets encountered icing conditions suitable for the external environment, the relevant parts of the body will freeze, making the aircraft's aerodynamic performance deterioration, severe endanger flight safety, in addition, the aircraft parked in the open winter months , there will be icing, you need to clean up before takeoff. We should grasp the mechanism of aircraft icing, environmental factors and easy to freeze parts of the body. This paper presents a simulation using the wind tunnel icing device icing wind tunnel simulations can reproduce t
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Procházka, Jaromír, and Ivana Procházková. "Icing Operations - De-Icing Policy." MAD - Magazine of Aviation Development 1, no. 4 (2013): 8. http://dx.doi.org/10.14311/mad.2013.04.02.

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The accumulation of ice, frost and snow on aircraft surfaces can drastically reduce the climb and maneuvering capabilities of an aircraft. The removal of such contamination prior to take off MUST be strictly adhered to in accordance with regulations and standards. The policy with respect to aircraft icing contamination should be “MAKE IT CLEAN AND KEEP IT CLEAN”. All personnel associated with the dispatch and/or operation of aircraft share the responsibility for ensuring that no aircraft is dispatched unless it is clear of ice, snow or frost.
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Wang, Kang, Yuan Xue, Hongfeng Tian, Miaosen Wang, and Xiaolong Wang. "The Impact of Icing on the Airfoil on the Lift-Drag Characteristics and Maneuverability Characteristics." Mathematical Problems in Engineering 2021 (June 12, 2021): 1–16. http://dx.doi.org/10.1155/2021/5568740.

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Icing has now become an important factor endangering flight safety. This paper takes the icing data of the NACA 23012 airfoil as an example, establishes an icing influence model for real-time simulation based on icing time and aircraft angle of attack, and analyzes the influence of different icing geometry on aircraft characteristics. The two-dimensional interpolation method is used to improve the model of the aircraft’s stall area, which is mainly divided into the correction of the lift-drag coefficient linear area and the stall area and the correction of the aircraft stability derivative and
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Elfitra Desifatma. "Electrical Wing Prototype Anti Icing pada Pesawat Komersil." Jurnal Jaring SainTek 2, no. 2 (2020): 34–41. http://dx.doi.org/10.31599/jaring-saintek.v2i2.331.

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The accumulation of ice on the aircraft's wings can cause a decrease in the aerodynamic properties of the aircraft, increase in weight, and it is difficult to control the aircraft so that it affects aircraft safety. Icing handling on aircraft is growing. One of the newest systems being developed is electrical anti-icing. Therefore, the researcher designed a prototype of an anti-icing electrical wing on a commercial aircraft with advantages in terms of maintenance and lighter components. The purpose of making this prototype is to design an anti-icing electrical wing in the form of a prototype a
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Gent, R. W., N. P. Dart, and J. T. Cansdale. "Aircraft icing." Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences 358, no. 1776 (2000): 2873–911. http://dx.doi.org/10.1098/rsta.2000.0689.

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Amelyushkin, I. A., M. A. Kudrov, and P. S. Kuleshov. "Peculiarities of icing in a flow with supercooled droplets and ice crystals." Journal of Physics: Conference Series 2817, no. 1 (2024): 012025. http://dx.doi.org/10.1088/1742-6596/2817/1/012025.

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Abstract New results of aircraft icing are obtained. New mathematical models of physical phenomena are formulated. Original construction of adaptive wing was invented, developed and prototypes were built. New algorithm of aircrafts’ surface with nanorelief are developed. Parametric studies of aircraft icing peculiarities were carried out.
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Ruan, Qikang. "Analysis of the types of aircraft icing and the solutions." Applied and Computational Engineering 9, no. 1 (2023): 177–81. http://dx.doi.org/10.54254/2755-2721/9/20230082.

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Aircraft ice accumulation has a negative impact on flight safety, the smooth flow field on the aircraft surface, flight drag, flight control accuracy, and lift. It interferes with the smooth flow field of the aircraft's surface, increases flight drag, lessens the accuracy of the flight controls, diminishes the lift of the aircraft, and affects the stability and operation of the aircraft. The primary scientific challenge is to catalog the several forms of icing that exist, along with their sources and aerodynamic configuration-related impacts. This paper primarily examines the most efficient de
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Yue, Ting, Xianlong Wang, Bo Wang, et al. "Design of Ice Tolerance Flight Envelope Protection Control System for UAV Based on LSTM Neural Network for Detecting Icing Severity." Drones 9, no. 1 (2025): 63. https://doi.org/10.3390/drones9010063.

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Icing on an unmanned aerial vehicle (UAV) can degrade aerodynamic performance, reduce flight capabilities, impair maneuverability and stability, and significantly impact flight safety. At present, most flight control methods for icing-affected aircraft adopt a conservative control strategy, in which small control inputs are used to keep the aircraft’s angle of attack and other state variables within a limited range. However, this approach restricts the flight performance of icing aircraft. To address this issue, this paper innovatively proposes a design method of an ice tolerance flight envelo
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Liu, Huan, Yi Wang, Li Lei, Zheyuan Liu, and Xindang He. "A prediction method for aircraft icing severity forecast based on probability model and meteorological observation data." Journal of Physics: Conference Series 2762, no. 1 (2024): 012011. http://dx.doi.org/10.1088/1742-6596/2762/1/012011.

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Abstract Aircraft flight performance and safety are inevitably affected by adverse meteorological conditions, one such weather is icing. Aircraft icing can cause severe aerodynamic and flight mechanical effects, thus threatens aircraft flight safety. This study presents an aircraft icing severity prediction method with probabilistic model, in which meteorological observation data are described as random variables and the airplane icing severity level is defined as fuzzy variables with membership function. When the information of aircraft flying cloud type, altitude, speed, temperature, pressur
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Dissertations / Theses on the topic "Aircraft icing"

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Ma, Qinglin. "Aircraft icing and thermo-mechanical expulsion de-icing technology." Thesis, Cranfield University, 2010. http://dspace.lib.cranfield.ac.uk/handle/1826/12478.

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The topic of this thesis is Aircraft Icing and Aircraft Icing and Thermo-Mechanical Expulsion De-icing Technology. The main objectives are to investigate aircraft icing meteorology and effects on aircraft, ice protection systems and thermo-mechanical expulsion de-icing technology. Initially, the research project focuses on aircraft icing meteorology, ice accumulation and icing effects on flight safety. A basic understanding of aircraft icing is explained, including icing conditions and parameters, ice detection, ice accretion shapes, and icing effects in terms of different airframe surfaces. I
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Wang, Yuchen. "Development of improved aircraft de-icing fluids." Thesis, University of Strathclyde, 2013. http://oleg.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=25541.

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Turcotte, François A. "A method for aircraft icing diagnosis in precipitation /." Thesis, McGill University, 1994. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=55400.

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A study of feasibility is performed for the development of a nowcasting method of aircraft icing conditions. The supercooled cloud water content is a key parameter for the determination of hazardous regions. The production of supercooled water in clouds is possible only where sufficiently strong updraft produces supersaturation with respect to water. However, to maintain the presence of supercooled droplets, the generation of moisture excess during the air uplift must exceed the rate of vapor deposition on snow and the rate of snow riming. The "storm of the century" (March 13-14, 1993) has bee
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Matheis, Brian Daniel. "Numerical investigation of roughness effects in aircraft icing calculations." [Ames, Iowa : Iowa State University], 2008.

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Leese, Graeme Neil. "On the accretion of ice on aircraft." Thesis, University of Cambridge, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.609639.

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Charpin, Jean P. F. "Water flow on accreting ice surfaces." Thesis, Cranfield University, 2002. http://dspace.lib.cranfield.ac.uk/handle/1826/10742.

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Ice growth may rapidly degrade the aerodynamic performance of an aircraft. It can also severely damage structures such as communication towers or power lines. Subsequently, de-icing and anti-icing systems have been developed and a number of codes designed to predict ice shapes. When ice accretion starts, two different types of ice can appear, depending on the temperature and conditions. All of the incoming fluid may freeze almost instantaneously and turn into rime ice. Alternatively, a fraction of the incoming fluid may freeze and turn into glaze ice while the other part remains liquid and may
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Zeppetelli, Danial. "Computational fluid dynamics icing analysis: a predictive approach to in-flight icing risk management and aircraft certification." Thesis, McGill University, 2011. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=104598.

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In-flight icing is a hazard that continues to afflict the aviation industry, despite all the research and efforts to mitigate the risks. The recurrence of these types of accidents has given renewed impetus to the development of advanced analytical predictive tools to study both the accretion of ice on aircraft components in flight, and the aerodynamic consequences of such ice accumulations. In this work, an in-depth analysis of the occurrence of in-flight icing accidents and incidents was conducted to identify high-risk flight conditions. To investigate these conditions more thoroughly, a comp
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Erdogan, Baris. "Production And Development Of De/anti Icing Fluids For Aircraft." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/3/12609926/index.pdf.

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Aircraft are not allowed to take off prior to cleaning of snow and ice deposits that form on their surfaces under winter conditions to refrain from compromising flight safety. Water based solutions containing mainly ethylene or propylene glycol, or both, are employed either to remove the snow/ice layers or to provide protection against deposition of these layers. The first group of solutions, i.e. de-icing fluids, are Newtonian and have generally low viscosity so that right after their application they fall off the aircraft surfaces, providing little or no further protection against precipitat
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Pellissier, Mathieu. "Optimization via CFD of aircraft hot-air anti-icing systems." Thesis, McGill University, 2010. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=95154.

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In-flight icing is a major concern in aircraft safety and a non-negligible source of incidents and accidents, and is still a serious hazard today. It remains consequently a design and certification challenge for aircraft manufacturers. The aerodynamic performance of an aircraft can indeed degrade rapidly when flying in icing conditions, leading to incidents or accidents. In-flight icing occurs when an aircraft passes through clouds containing supercooled water droplets at or below freezing temperature. Droplets impinge on its exposed surfaces and freeze, causing roughness and shape changes tha
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Anderson, Harry. "Stability effects of heat and mass transfer on thin liquid films." Thesis, Cranfield University, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.250500.

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Books on the topic "Aircraft icing"

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Shaw, Robert J. NASA's aircraft icing analysis. National Aeronautics and Space Administration, 1986.

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Lankford, Terry T. Aircraft icing: A pilot's guide. McGraw-Hill, 2000.

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United States. National Aeronautics and Space Administration., ed. NASA's aircraft icing technology program. National Aeronautics and Space Administration, 1991.

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United States. Office of Federal Coordinator for Meteorological Services and Supporting Research, ed. National aircraft icing technology plan. U.S. Dept. of Commmerce, National Oceanic and Atmospheric Administration, 1986.

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Civil Aviation Authority. Ground de-icing of aircraft. Civil Aviation Authority, 1985.

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Bachalo, W. D. Advanced instrumentation for aircraft icing research. National Aeronautics and Space Administration, 1990.

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Sweeney, Hugh J. Some microphysical processes affecting aircraft icing: Final report. Atmospheric Sciences Division, Air Force Geophysics Laboratory, 1985.

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Organisation, International Civil Aviation. Manual of aircraft ground de/anti-icing operations. International Civil Aviation Organisation, 1995.

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Anderson, David N. Scaling methods for simulating aircraft in-flight icing encounters. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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Foss, Van Zante Judith, Sim Alex, and NASA Glenn Research Center, eds. NASA/FAA Tailplane Icing Program: Flight test report. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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Book chapters on the topic "Aircraft icing"

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Purvis, Richard, and Frank T. Smith. "Improving Aircraft Safety in Icing Conditions." In UK Success Stories in Industrial Mathematics. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-25454-8_19.

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Wang, Liwen, Hongzhen Yang, and Bin Chen. "Multi-Information Integration System of Aircraft Ground Concentrated De-icing." In Lecture Notes in Electrical Engineering. Springer London, 2013. http://dx.doi.org/10.1007/978-1-4471-4856-2_108.

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Xu, Wu, and Li Jinjian. "Assessment of Forecast Algorithms of Aircraft Icing in Southwestern China." In Smart Innovation, Systems and Technologies. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-1781-4_12.

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De Gennaro, Michele, James Page, Isik Ozcer, Guillaume Moula, Salvatore Corcione, and Vincenzo Cusati. "Advances on the Next Generation Short-Medium Range Aircraft Rear End: The CleanSky 2 Project IMPACT." In Lecture Notes in Mobility. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-89444-2_15.

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Abstract This paper aims at presenting the results of the CleanSky 2 European project IMPACT (GA no. 885052), granted under the Large Passenger Aircraft Integrated Technology Demonstrator (LPA-ITD), aiming at optimizing the rear-end design for the next generation Short and Medium Range (SMR) A320-like aircraft. Specifically, the project has investigated a Forward Swept Horizontal Tail Plane (FSHTP) enhanced with a Leading-Edge eXtension (LeX) device. The activities have focused on the optimisation of the horizontal stabilizer, accounting for the coupled aerodynamic, aeroelastic and, for the fi
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Douxchamps, Benoit, Laurent Lannot, Natacha Najac, and Thomas Renault. "Numerical Simulation for Supplemental Type Certification of Aircraft Flying into Known Icing." In Handbook of Numerical Simulation of In-Flight Icing. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-33845-8_35.

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Douxchamps, Benoit, Laurent Lannot, Natacha Najac, and Thomas Renault. "Numerical Simulation for Supplemental Type Certification of Aircraft Flying into Known Icing." In Handbook of Numerical Simulation of In-Flight Icing. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-030-64725-4_35-1.

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Zhan, Zhao, and Wagdi G. Habashi. "Numerical Simulation of Aircraft and Rotorcraft In-Flight Icing via Reduced Order Models." In Handbook of Numerical Simulation of In-Flight Icing. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-33845-8_36.

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Zhan, Zhao, and Wagdi G. Habashi. "Numerical Simulation of Aircraft and Rotorcraft In-Flight Icing via Reduced Order Models." In Handbook of Numerical Simulation of In-Flight Icing. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-030-64725-4_36-1.

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Hu, Hui. "Development of Advanced Flow Diagnostic Techniques to Characterize Aircraft Icing Phenomena." In Progress in Hybrid RANS-LES Modelling. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-27607-2_2.

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Tserpes, Konstantinos, Elli Moutsompegka, Mareike Schlag, et al. "Characterization of Pre-bond Contamination and Aging Effects for CFRP Bonded Joints Using Reference Laboratory Methods, Mechanical Tests, and Numerical Simulation." In Adhesive Bonding of Aircraft Composite Structures. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_2.

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AbstractIn this chapter, the pre-bond contamination and ageing effects on carbon fiber reinforced plastic (CFRP) adherends and CFRP bonded joints are characterized by means of reference laboratory non-destructive testing (NDT) methods, mechanical tests, and numerical simulation. Contaminations from two fields of application are considered, namely in aircraft manufacturing (i.e. production) and for in-service bonded repair. The production-related scenarios comprise release agent, moisture, and fingerprint, while the repair-related scenarios comprise fingerprint, thermal degradation, de-icing fl
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Conference papers on the topic "Aircraft icing"

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Bragg, Michael B., Tamer Basar, William R. Perkins, et al. "Smart Icing Systems for Aircraft Icing Safety." In FAA In-flight Icing / Ground De-icing International Conference & Exhibition. SAE International, 2003. http://dx.doi.org/10.4271/2003-01-2100.

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Bragg, M., T. Basar, W. Perkins, et al. "Smart icing systems for aircraft icing safety." In 40th AIAA Aerospace Sciences Meeting & Exhibit. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-813.

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HINKELMAN, JR., JOHN. "Improving aircraft icing forecasts." In 25th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-532.

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Ryerson, Charles. "Aircraft icing remote sensing." In 36th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-578.

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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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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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Müller, Nicolas Carlo, and Richard Hann. "UAV Icing: 3D Simulations of Propeller Icing Effects and Anti-Icing Heat Loads." In International Conference on Icing of Aircraft, Engines, and Structures. SAE International, 2023. http://dx.doi.org/10.4271/2023-01-1383.

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<div class="section abstract"><div class="htmlview paragraph">In-flight atmospheric icing is a significant threat to the use of unmanned aerial vehicles (UAVs) in adverse weather. The propeller of the UAV is especially sensitive to icing conditions, as it accumulates ice at a faster rate than the wings of the UAVs. Ice protection systems can be developed to counteract the danger of icing on the propeller of UAVs. In this study, the influence of different meteorological conditions on a propeller of a UAV is analyzed for a UAV with a wingspan of a few meters. The ice accretion and th
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Zlotky, Gail M. "Aircraft Ground Deicing: An Automated Approach." In FAA In-flight Icing / Ground De-icing International Conference & Exhibition. SAE International, 2003. http://dx.doi.org/10.4271/2003-01-2116.

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Ribbens, William B. "Detection of Ice on Aircraft Tail Surfaces." In FAA In-flight Icing / Ground De-icing International Conference & Exhibition. SAE International, 2003. http://dx.doi.org/10.4271/2003-01-2112.

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ADAMS, RICHARD. "Aircraft icing certification - In perspective." In 26th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-204.

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Reports on the topic "Aircraft icing"

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Cornell, Daniel, Christopher A. Donahue, and Chan Keith. A Comparison of Aircraft Icing Forecast Models. Defense Technical Information Center, 1995. http://dx.doi.org/10.21236/ada305466.

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Baca, Al, and Carroll Herring. Minutes of Aircraft/Runway Deicing/Anti-Icing Technology Crossfeed. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada315985.

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Davis, Matthew C. New Ionic Liquids from Natural Products for Environmentally Benign Aircraft Deicing and Anti-Icing. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada580819.

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Chauhan, S. P., M. S. Roshon, W. D. Samuels, and E. S. Berman. Environmentally Benign Aircraft Anti-icing and Deicing Fluids Based on Cost Effective, Bio-based Ingredients. Defense Technical Information Center, 2012. http://dx.doi.org/10.21236/ada572809.

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