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Relevant bibliographies by topics / Icing of aerodynamic surfaces

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Academic literature on the topic 'Icing of aerodynamic surfaces'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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Journal articles on the topic "Icing of aerodynamic surfaces"

1

Ma, Liqun, Zichen Zhang, Linyue Gao, Yang Liu, and Hui Hu. "Bio-Inspired Icephobic Coatings for Aircraft Icing Mitigation: A Critical Review." Reviews of Adhesion and Adhesives 8, no. 2 (2020): 168–99. http://dx.doi.org/10.7569/raa.2020.097307.

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A critical review is provided to summarize our recent efforts to utilize the state-of-the-art bio-inspired icephobic coatings/surfaces, i.e., 1). Lotus-leaf-inspired superhydrophobic surfaces (SHS) and 2). Pitcher-plant-inspired slippery liquid-infused porous surfaces (SLIPS) for aircraft icing mitigation. By leveraging the unique Icing Research Tunnel of Iowa State University (i.e., ISU-IRT), an experimental campaign was performed to evaluate the effectiveness of using SHS and SLIPS coatings to suppress impact ice accretion over the surfaces of typical airfoil/wing models. While both SHS and

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Akhazhanov, Sungat, and Sergey Skorobogatov. "CONDITIONS FOR THE OCCURRENCE OF ICING ON AERODYNAMIC PROFILES AND METHODS OF THEIR CALCULATION." Herald of Kazakh-British technical university 18, no. 2 (2021): 20–25. http://dx.doi.org/10.55452/1998-6688-2021-18-2-20-25.

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This article analyzes the methods and models suitable for studying the icing of the aerodynamic surface (wing). Systems to counteract the unifying effect are considered. Methods and models for calculating ice formations on aerodynamic surfaces are studied. Further study of the effect of icing will be conducted in the light of the characteristics of flow around bodies of viscous compressible medium in terms of load and liquid phase in case of changes in the geometric parameters of the bodies and reflect this change in the external stream.

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Knyaz, V. A., E. V. Ippolitov, and M. M. Novikov. "3D RECONSTRUCTION OF ICE SHAPE USING VISIBLE AND THERMAL RANGE IMAGING FOR AIRCRAFT ICING STUDY." International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences XLIII-B2-2021 (June 28, 2021): 527–32. http://dx.doi.org/10.5194/isprs-archives-xliii-b2-2021-527-2021.

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Abstract. Aircraft icing is one of the main factors decreasing the flight safety. Qualitative and quantitative understanding of the icing process is crucially needed for developing anti-icing measures and safety recommendations. Changes in aerodynamic characteristics of aircraft caused by changes in shape of aircraft surfaces due to the ice accretion can lead to significant aerodynamic performance degradation. So the reliable and accurate information of how the shape of the ice accretion influences on aerodynamic characteristics is a key point for predicting the changes in aerodynamic performa

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Xia, Annan, Lei He, Shihang Qie, et al. "Fabrication of an Anti-Icing Aluminum Alloy Surface by Combining Wet Etching and Laser Machining." Applied Sciences 12, no. 4 (2022): 2119. http://dx.doi.org/10.3390/app12042119.

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The phenomenon of icing on the surface of the fuselage while aircraft pass through clouds has an impact on flight safety. This aircraft icing may adversely affect metrological conditions and cause aerodynamic mechanical effects, resulting in a threat to flight safety. This research aims to fabricate an anti-icing surface on a 2524 aluminum alloy material by combining laser machining and wet etching. The microstructure surfaces were obtained by laser, the nanostructured surfaces were obtained by wet etching, and the hierarchical structures were prepared through a combination of these two proces

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Moghtadernejad, S., M. Jadidi, N. Esmail, and A. Dolatabadi. "Shear-driven droplet coalescence and rivulet formation." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 230, no. 5 (2015): 793–803. http://dx.doi.org/10.1177/0954406215590186.

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Icing on aerodynamic surfaces occurs due to the accumulation of rain droplets when the surrounding temperature is below the freezing temperature. It is well known that icing phenomenon alters the aircraft aerodynamic forces and may cause serious damage. Therefore, studying water droplet behavior, such as shedding and coalescence serves as the primary step which can lead to understanding the fundamental physics of aircraft icing. Hence, in this study an experimental approach is used to investigate the shear-driven droplet shedding and coalescence on a hydrophilic substrate which can serve as th

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Pan’kov, A. A., and P. V. Pisarev. "Anti-icing indicator polymer coating with built-in fiber-optic PEL-sensor for indication, location and de-icing of aerodynamic surfaces." PNRPU Mechanics Bulletin, no. 4 (December 15, 2021): 111–21. http://dx.doi.org/10.15593/perm.mech/2021.4.11.

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A mathematical model was developed and a numerical modal analysis of the anti-icing mode of operation of the new indicator polymer coating with an integrated optical fiber piezoelectroluminescent (PEL) sensor for icing indication, location and self-cleaning from icing of aerodynamic surfaces was given. The fiber optic PEL-sensor is located in the plane of the coating. Receiver-analyzer of informative integral intensities of light signals is installed at output from optical fiber of sensor. Alternating voltage generator is connected to outputs of two control electrodes of sensor. The anti-icing

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Fukudome, Koji, Yuki Tomita, Sho Uranai, Hiroya Mamori, and Makoto Yamamoto. "Evaluation of Anti-Icing Performance for an NACA0012 Airfoil with an Asymmetric Heating Surface." Aerospace 8, no. 10 (2021): 294. http://dx.doi.org/10.3390/aerospace8100294.

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Heating devices on airfoil surfaces are widely used as an anti-icing technology. This study investigated the aerodynamic performance with a static heating surface based on the modified extended Messinger model. The predicted ice shape was validated through a comparison with the experimental results for HAARP-II. A reasonable agreement was found for both the icing area and the ice mass on the suction surface. Then, the prediction method was adopted for an NACA0012 airfoil at an attack angle of 4.0∘ under a glaze ice condition. An asymmetric heating area was imposed on the suction and pressure s

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Fürbacher, Roland, Gerhard Liedl, Gabriel Grünsteidl, and Andreas Otto. "Icing Wind Tunnel and Erosion Field Tests of Superhydrophobic Surfaces Caused by Femtosecond Laser Processing." Wind 4, no. 2 (2024): 155–71. http://dx.doi.org/10.3390/wind4020008.

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Ice accumulation on lift-generating surfaces, such as rotor blades or wings, degrades aerodynamic performance and increases various risks. Active measures to counteract surface icing are energy-consuming and should be replaced by passive anti-icing surfaces. Two major categories of surface treatments—coating and structuring—already show promising results in the laboratory, but none fulfill the current industry requirements for performance and durability. In this paper, we show how femtosecond laser structuring of stainless steel (1.4301) combined with a hydrocarbon surface treatment or a vacuu

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Milles, Stephan, Vittorio Vercillo, Sabri Alamri, et al. "Icephobic Performance of Multi-Scale Laser-Textured Aluminum Surfaces for Aeronautic Applications." Nanomaterials 11, no. 1 (2021): 135. http://dx.doi.org/10.3390/nano11010135.

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Ice-building up on the leading edge of wings and other surfaces exposed to icing atmospheric conditions can negatively influence the aerodynamic performances of aircrafts. In the past, research activities focused on understanding icing phenomena and finding effective countermeasures. Efforts have been dedicated to creating coatings capable of reducing the adhesion strength of ice to a surface. Nevertheless, coatings still lack functional stability, and their application can be harmful to health and the environment. Pulsed laser surface treatments have been proven as a viable technology to indu

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Milles, Stephan, Vittorio Vercillo, Sabri Alamri, et al. "Icephobic Performance of Multi-Scale Laser-Textured Aluminum Surfaces for Aeronautic Applications." Nanomaterials 11, no. 1 (2021): 135. http://dx.doi.org/10.3390/nano11010135.

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Ice-building up on the leading edge of wings and other surfaces exposed to icing atmospheric conditions can negatively influence the aerodynamic performances of aircrafts. In the past, research activities focused on understanding icing phenomena and finding effective countermeasures. Efforts have been dedicated to creating coatings capable of reducing the adhesion strength of ice to a surface. Nevertheless, coatings still lack functional stability, and their application can be harmful to health and the environment. Pulsed laser surface treatments have been proven as a viable technology to indu

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Dissertations / Theses on the topic "Icing of aerodynamic surfaces"

1

Lewis, G. J. "De-icing of aerodynamic surfaces using electromechanical impulses." Thesis, University of Nottingham, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.372486.

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Szolnoky, Ramos Pinto Cunha Filipe. "Mechanism of flow of de/anti-icing fluid film on a wing surface and effects on aerodynamic performances." Doctoral thesis, Universite Libre de Bruxelles, 2001. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/211551.

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Heydari, Golrokh. "Toward Anti-icing and De-icing Surfaces : Effects of Surface Topography and Temperature." Doctoral thesis, KTH, Yt- och korrosionsvetenskap, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-186187.

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Icing severely affects society, especially in the Nordic countries. Iceaccumulation can result in critical performance problems and safetyconcerns for instance in road, air and sea transportation, transmissionlines, marine and offshore structures, wind turbines and heat exchangers.Present active ice-combating approaches possess environmental,efficiency and cost drawbacks. Thus, fabricating icephobic surfaces orcoatings impeding ice formation (anti-icing), but facilitating ice removal(de-icing) is desired. However, different conditions in the environmentduring ice formation and growth add to th

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Kepets, Mark Alexander 1978. "Actively conformable aerodynamic surfaces." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/82226.

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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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Chanda, Jagannath, Leonid Ionov, Alina Kirillovaab, and Alla Synytska. "New insight into icing and de-icing properties of hydrophobic and hydrophilic structured surfaces based on core–shell particles." Royal Society of Chemistry, 2015. https://tud.qucosa.de/id/qucosa%3A36410.

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Icing is an important problem, which often leads to emergency situations in northern countries. The reduction of icing requires a detailed understanding of this process. In this work, we report on a systematic investigation of the effects of geometry and chemical properties of surfaces on the formation of an ice layer, its properties, and thawing. We compare in detail icing and ice thawing on flat and rough hydrophilic and hydrophobic surfaces. We also show advantages and disadvantages of the surfaces of each kind. We demonstrate that water condenses in a liquid form, leading to the formation

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Collu, Maurizio. "Dynamics of marine vehicles with aerodynamic surfaces." Thesis, Cranfield University, 2008. http://dspace.lib.cranfield.ac.uk/handle/1826/7022.

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An assessment of the relative speeds and payload capacities of airborne and waterborne vehicles highlights a gap which can be usefully filled by a new vehicle concept, utilizing both hydrodynamic and aerodynamic forces. A high speed marine vehicle equipped with aerodynamic surfaces (called an AAMV, 'Aerodynamically Alleviated Marine Vehicle') is one such concept. The development of this type of vehicle requires a mathematical framework to characterize its dynamics taking account of both aerodynamic and hydrodynamic forces. This thesis presents the development of unified and consistent equation

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Insana, Eric J. "Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions." University of Dayton / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1597082782224451.

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Streitz, Jeffrey Thomas Jr. "A windtunnel study of thin-sheet and rivulet icing formation on planar surfaces." Thesis, University of Iowa, 1999. https://ir.uiowa.edu/etd/5095.

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Standingford, David William Fin. "Optimal lifting surfaces, including end plates, ground effect & thickness /." Title page, contents and abstract only, 1997. http://web4.library.adelaide.edu.au/theses/09PH/09phs785.pdf.

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Books on the topic "Icing of aerodynamic surfaces"

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Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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Foss, Van Zante Judith, and Lewis Research Center, eds. In-flight aerodynamic measurements of an iced horizontal tailplane. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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Center, NASA Glenn Research, ed. An evaluation of an analytical simulation of an airplane with tailplane icing by comparision to flight data. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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5

Shaw, Robert J. Predictions if airfoil aerodynamic performance degradation due to icing. National Aeronautics and Space Administration, 1989.

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Ratvasky, Thomas P. NASA/FAA Tailplane Icing Program overview. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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Foss, Van Zante Judith, Riley James T, Lewis Research Center, and United States. National Aeronautics and Space Administration., eds. NASA/FAA Tailplane Icing Program overview. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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8

Barger, Raymond L. Semianalytic modeling of aerodynamic shapes. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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9

Allen, Arrington E., American Institute of Aeronautics and Astronautics., NASA Glenn Research Center, and Aerospace Sciences Meeting & Exhibit (36th : 1998 : Reno, Nev.), eds. Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests). National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Center, NASA Glenn Research, ed. Ice accretions and icing effects for modern airfoils. National Aeronautics and Space Administration, Glenn Research Center, 2000.

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Book chapters on the topic "Icing of aerodynamic surfaces"

1

Zheng, Yongmei. "Anti-Icing/Icephobic Surfaces." In Bioinspired Materials Surfaces. Jenny Stanford Publishing, 2024. http://dx.doi.org/10.1201/9781003513889-4.

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Zhu, Weixin, Tengfei Xiang, Yizhou Shen, Lingfeng Zhao, and Xuefeng Nong. "Slippage Interface on Lubricious Surfaces." In Icephobic Materials for Anti/De-icing Technologies. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-6293-4_4.

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Shen, Yizhou, Xuefeng Nong, Tengfei Xiang, Lingfeng Zhao, and Aituhan Yeerken. "Ice Adhesion on Lubricious Surfaces." In Icephobic Materials for Anti/De-icing Technologies. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-6293-4_10.

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Amirfazli, Alidad, and Carlo Antonini. "CHAPTER 11. Fundamentals of Anti-Icing Surfaces." In Soft Matter Series. Royal Society of Chemistry, 2016. http://dx.doi.org/10.1039/9781782623953-00319.

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Shaw, Robert J., Mark G. Potapczuk, and Colin S. Bidwell. "Predictions of Airfoil Aerodynamic Performance Degradation Due to Icing." In Numerical and Physical Aspects of Aerodynamic Flows IV. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-662-02643-4_2.

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Zhou, Enqi, Yizhou Shen, Aituhan Yeerken, Jiawei Jiang, and Xuefeng Nong. "Ice Adhesion on Superhydrophobic Micro-Nanostructure Surfaces." In Icephobic Materials for Anti/De-icing Technologies. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-6293-4_9.

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Shen, Yizhou, Zhaoru He, Xinyu Xie, et al. "Non-Wetting Interface on Micro-Nanostructure Surfaces." In Icephobic Materials for Anti/De-icing Technologies. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-6293-4_3.

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Zhu, Weixin, Yingxuan Jia, Yizhou Shen, Xu Fu, and Zhaoru He. "Water-Film Flowing Control on the Solid Surfaces." In Icephobic Materials for Anti/De-icing Technologies. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-6293-4_5.

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Humphreys, Bryan E., and Ernst J. Totland. "Saab 2000 In-Service Test of Porous Surfaces for HLFC." In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_11.

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Mahrt, L. "The Bulk Aerodynamic Formulation over Heterogeneous Surfaces." In Boundary-Layer Meteorology 25th Anniversary Volume, 1970–1995. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-017-0944-6_5.

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Conference papers on the topic "Icing of aerodynamic surfaces"

1

Thomaier, Rob, and Danielle Peak. "Ice-Phobic Coatings for Wind Tower Blades and Structures." In SSPC 2013 Greencoat. SSPC, 2013. https://doi.org/10.5006/s2013-00069.

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Abstract Ice build-up on wind power blades can affect efficiency by reducing the aerodynamics of the blades. The sudden release of ice through centripetal force can result in dangerous projectiles in the large chunks of released ice. Moreover, icing can add additional mass to the turbine structure, causing stress on supporting members and shortening the structure’s life span—strains which can culminate in catastrophic failure. Ice-phobic coatings aid in the release of ice and can even reduce ice build-up. A variety of test methods were used to test ice adhesion: the Zero Degree Cone test, a mo

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Palacios, Jose, Joseph Szefi, Douglas Wolfe, and Matthew Bailey. "Ice Testing of a Centrifugally Powered Pneumatic Deicing System for Helicopter Rotor Blades." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9662.

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A novel pneumatic approach to protect helicopter rotor blades from ice accretion is presented in this paper. The system relies on centrifugally generated pressures to deform a 0.508 mm (0.02 in.) thick titanium leading edge cap. The leading edge cap is protected by a 10 μm (390 microinch) thick Ti-Al-N erosion resistant coating. Beneath the titanium leading edge, six (6) pneumatic diaphragms were installed. The diaphragms are normally deflated under vacuum against the surface of the blade, and are inflated when ice accretion thickness reaches a critical value. The deformation of the leading ed

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Karli, Geoffrey, Sihong Yan, and Jose Palacios. "Full-Scale EVTOL Rotor Icing Wind Tunnel Testing." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-0034.

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In recent years, the electrically powered Urban Air Mobility (UAM) market has witnessed significant growth, fueled by advances in electric motor and high-power-density lithium battery technologies. This surge of interest has prompted an exploration into the design and functionality of electric vertical take-off and landing (eVTOL) vehicles, particularly those with multi-tilt-rotor configurations. These eVTOL vehicles, capable of operating at higher RPMs than traditional helicopters, face unique challenges, especially under adverse environmental conditions such as icing. Aircraft airframe icing

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Xiao, Sid, David Belt, Pietro D'Ettorre, and Paul Edwards. "Control Margin Awareness of the AW609 TiltRotor under Asymmetric Aerodynamic Flight Conditions." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0074-2018-12791.

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The ability to model and evaluate aircraft performance prior to flight has generated a significant increase in safety margin in the flight testing of experimental aircraft. Prior to the artificial icing campaign for the AW609 aircraft, a flight model of predicted aerodynamic behavior was used to rapidly generate a control margin monitoring and warning system, which was implemented on-board the aircraft during testing to provide awareness of predicted aircraft behavior under icing conditions.

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Yongsheng, Shi, and Xiang Yuhang. "Improved DETR-Based Detection of Icing and Snow on Aircraft Surfaces." In The International Conference on Data Mining, E-Learning, and Information Systems. SCITEPRESS - Science and Technology Publications, 2024. http://dx.doi.org/10.5220/0012877900004536.

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Duncan, Kristen, Stephen B. Gibson, and Wanda Goulden. "Corrosion Effects of Municipal Anti-icing and De-icing Programs." In CORROSION 2020. NACE International, 2020. https://doi.org/10.5006/c2020-14886.

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Abstract Anti-icing and de-icing chemicals are commonly used for winter road maintenance in areas that experience icy conditions. Anti-icing is a preventative strategy, while de-icing is a reactive strategy. In many jurisdictions, these two strategies are used in combination to improve the overall effectiveness of winter road maintenance programs. The City of Edmonton currently utilizes a combination of sodium chloride and sand as a de-icing program. To improve the economics and effectiveness of the overall winter road maintenance program, the City of Edmonton began a pilot program that utiliz

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Choo, Y. K., M. B. Vickerman, A. W. Hackenberg, and D. L. Rigby. "An Aerodynamic Simulation Process for Iced Lifting Surfaces and Associated Issues." In FAA In-flight Icing / Ground De-icing International Conference & Exhibition. SAE International, 2003. http://dx.doi.org/10.4271/2003-01-2135.

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Okulova, N., R. Taboryski, J. N. Sørensen, S. I. Shtork, and V. L. Okulov. "Aerodynamic effect of icing/rain impacts on super-hydrophobic surfaces." In INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2018). Author(s), 2018. http://dx.doi.org/10.1063/1.5065139.

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Bartkus, Tadas, Sam Lee, and Eric Stewart. "Icing Physics Studies Using the 3D SIDRM Test Article: Aerodynamic and Supercooled Liquid Icing Analysis." In International Conference on Icing of Aircraft, Engines, and Structures. SAE International, 2023. http://dx.doi.org/10.4271/2023-01-1399.

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<div class="section abstract"><div class="htmlview paragraph">In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation capability. Experimental data is required for development of icing physics models and simulation validation. To that end, this paper presents the analysis of the supercooled liquid icing data subset from tests conducted in 2022 at the NASA Icing Research Tunnel that studied both supercooled water and ice-crystal icing. The

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Monaco, Ernesto, Fabrizio Ricci, Vittorio Memmolo, Salvatore Ameduri, Antonio Concilio, and Leandro Maio. "Development of a de-icing system for aerodynamic surfaces based on ultrasonic waves." In Health Monitoring of Structural and Biological Systems XII, edited by Tribikram Kundu. SPIE, 2018. http://dx.doi.org/10.1117/12.2300780.

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Reports on the topic "Icing of aerodynamic surfaces"

1

Rockwell, Donald. Origin and Control of Unsteady Loading of Aerodynamic Surfaces Due to Vortex Breakdown and Stall. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada402569.

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Asenath-Smith, Emily, Emily Jeng, Emma Ambrogi, Garrett Hoch, and Jason Olivier. Investigations into the ice crystallization and freezing properties of the antifreeze protein ApAFP752. Engineer Research and Development Center (U.S.), 2022. http://dx.doi.org/10.21079/11681/45620.

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Antifreeze proteins (AFPs) allow biological organisms, including insects, fish, and plants, to survive in freezing temperatures. While in solution, AFPs impart cryoprotection by creating a thermal hysteresis (TH), imparting ice recrystallization inhibition (IRI), and providing dynamic ice shaping (DIS). To leverage these ice-modulating effects of AFPs in other scenarios, a range of icing assays were performed with AFPs to investigate how AFPs interact with ice formation when tethered to a surface. In this work, we studied ApAFP752, an AFP from the beetle Anatolica polita, and first investigate

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Lawson. L51597 Feasibility Study of New Technology for Intake Air Filtration. Pipeline Research Council International, Inc. (PRCI), 1989. http://dx.doi.org/10.55274/r0010105.

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Inlet air filters are widely used to remove solids and liquid droplets from the ambient air before it enters the compressor of a gas turbine. Clean inlet air provides many advantages: Less corrosion of the compressor and of gas-path hot parts, such as the turbine, decreased compressor fouling, less erosion of the compressor bladeThese in turn prevent deterioration of output and heat rate, and reduce maintenance costs. Compressor fouling is caused by the ingestion of substances that deposit and adhere to blade surfaces, resulting in reduced aerodynamic efficiency and decreased available output.

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Law, Edward, Samuel Gan-Mor, Hazel Wetzstein, and Dan Eisikowitch. Electrostatic Processes Underlying Natural and Mechanized Transfer of Pollen. United States Department of Agriculture, 1998. http://dx.doi.org/10.32747/1998.7613035.bard.

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The project objective was to more fully understand how the motion of pollen grains may be controlled by electrostatic forces, and to develop a reliable mechanized pollination system based upon sound electrostatic and aerodynamic principles. Theoretical and experimental analyses and computer simulation methods which investigated electrostatic aspects of natural pollen transfer by insects found that: a) actively flying honeybees accumulate ~ 23 pC average charge (93 pC max.) which elevates their bodies to ~ 47 V likely by triboelectrification, inducing ~ 10 fC of opposite charge onto nearby poll

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