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

Author: Grafiati

Published: 30 May 2022

Last updated: 31 July 2025

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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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2

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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3

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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4

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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5

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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6

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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7

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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8

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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9

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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10

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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11

Santos, Luis Carlos de Castro. "A hybrid inverse optimization method for aerodynamic design of lifting surfaces." Diss., Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/12105.

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12

Kondrashov, Vitaliy [Verfasser]. "Novel Silicon and Polymer Nanograss Surfaces - Generation, Wetting Properties and the Prevention of Icing / Vitaliy Kondrashov." München : Verlag Dr. Hut, 2015. http://d-nb.info/1071513036/34.

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13

Honohan, Andrew M. "The interaction of synthetic jets with cross flow and the modification of aerodynamic surfaces." Diss., Georgia Institute of Technology, 2003. http://hdl.handle.net/1853/20836.

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14

Charpentier, Thibaut V. J. "The heterogeneous ice nucleation properties of structured and chemically tailored surfaces for the development of novel anti-icing materials." Thesis, University of Leeds, 2012. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.589051.

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Preventing icing occurring in installations is an important challenge for many industries such as aviation, civil construction, high power transmission systems, or air-conditioning industries. Ice accretion costs money by reducing the efficiency of systems, and can, under some conditions, be a major hazard that could cost human lives. The most popular de-icing chemicals currently used (salts or glycol) are effective and relatively cheap; however they are hazardous to the environment and the waste treatment disposal can be expensive and time consuming. Another alternative is to turn to surface

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15

Boyle, Christopher. "Inviscid aerodynamic predictions of hypersonic elliptical projectiles : a comparative study of the effects of stabilizing surfaces /." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2000. http://handle.dtic.mil/100.2/ADA380851.

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Thesis (M.S. in Applied Mathematics)--Naval Postgraduate School, June 2000.<br>Thesis advisors: Neta, Beny ; Edge, Harris. "June 2000." AD-A380 851. Includes bibliographical references (p. 115-116). Also Available online.

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16

Baumann, Martin John. "An experimental investigation of the aerodynamic effects of roughness consisting of arrays of depressions in surfaces." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape8/PQDD_0007/MQ43336.pdf.

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17

Ahmed, Hamza Hafez Ahmed Anwar. "End-wall flow of a surface-mounted obstacle on a convex hump." Auburn, Ala., 2009. http://hdl.handle.net/10415/1946.

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18

Goldberg, Phil, Sabine Apelt, Dirk Spitzner, et al. "Icing Temperature Measurements of Water on Pyroelectric Single Crystals: Impact of Experimental Methods on the Degree of Supercooling." Elsevier, 2018. https://tud.qucosa.de/id/qucosa%3A30867.

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In our experiments, the icing temperature of small water volumes placed on different pyroelectric single crystals (SrxBa1−xNb2O6, LiNbO3, and LiTaO3) was determined using two measurement setups: (1) the sessile droplet and (2) ring system method. In the first method, a free-standing water droplet was exposed to several external factors in the air environment. This was found to lead to higher icing temperatures compared to the second method where the water was more isolated from external factors such as evaporation. In the second method, the material of the ring system was found to be an import

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19

Chechi, Florence Endres. "Design e avaliação aerodinâmica da topologia geométrica superficial de ventoinhas." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2014. http://hdl.handle.net/10183/110130.

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Este trabalho tem como eixo principal a avaliação experimental de texturas para superfícies de pás com intuito de aumentar a eficiência de ventoinhas de pequeno porte em relação às ventoinhas padrão (com pás lisas), através das variáveis também investigar de forma qualitativa o potencial de diferentes topologias no efeito estético. A ênfase está na modelagem de texturas para a superfície das pás de cada ventoinha, que foram trabalhadas a fim de diminuir a quantidade de escoamento de ar necessária para o funcionamento da mesma. Para os testes feitos, foi escolhida como base a ventoinha de um Co

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20

Raiyan, Asif. "Fundamentals of Liquid Interactions with Nano/Micro Engineered Surfaces at Low Temperatures." University of Toledo / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=toledo154471832751114.

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21

Liu, Haiying. "Interfacing comprehensive rotorcraft analysis with advanced aeromechanics and vortex wake models." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/22534.

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Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2008.<br>Committee Chair: Bauchau, Olivier; Committee Member: Armanios, Erian; Committee Member: Hodges, Dewey; Committee Member: Ruzzene, Massimo; Committee Member: Stallybrass, Michael.

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22

Alsabagh, Abdel Salam. "Effect of atmospheric ice accretion on the dynamic performance of wind turbine blades." Thesis, University of Hertfordshire, 2017. http://hdl.handle.net/2299/17990.

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Atmospheric icing presents serious challenges to the development of wind power of the wind energy industry in cold regions. The potential detrimental impact on the safe operation of wind turbines and the energy harvest hasn't been fully understood and requires further investigation. This thesis presents the research on icing profiles under different weather conditions and their impact on natural frequency, fatigue life, and lift and drag of the wind turbine blade. The research aims to develop a further understanding of the effect of atmospheric ice accretion on the structural integrity and aer

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23

Thiévenaz, Virgile. "Impact et solidification de gouttes d'eau." Thesis, Sorbonne université, 2019. https://tel.archives-ouvertes.fr/tel-03358455.

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Lorsqu’une goutte d’eau tombe sur une surface froide – dont la température est inférieure à 0◦C – elle se met à geler en même temps qu’elle s’étale. La solidification ralentit l’étalement de la goutte, facilite sa fragmentation en gouttelettes, entraîne la rétraction de la goutte, et donne une certaine forme à la goutte gelée. La nature de la surface froide est déterminante dans le processus de solidification. Sur la base du problème de Stefan, nous avons développé un modèle de dynamique de solidification, prenant en compte la diffusion thermique dans le substrat. Ce modèle apporte une meilleu

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24

Boopathy, Komahan. "Uncertainty Quantification and Optimization Under Uncertainty Using Surrogate Models." University of Dayton / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1398302731.

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25

Шмирьов, Володимир Федорович, та Volodymyr Fedorovych Shmyrov. "Наукові основи проектування та створення енергозалежних систем літаків транспортної категорії". Thesis, Національний авіаційний університет, 2020. https://er.nau.edu.ua/handle/NAU/44724.

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Дисертаційну роботу присвячено розробці наукових основ проектування та створення енергозалежних систем та комплексів сучасних літаків транспортної категорії з оптимізацією за еквівалентною масою, включаючи повітрозбірники. Закладено наукові основи проектування систем протиобмерзання літаків, починаючи від визначення зон захисту, потрібних енергетичних витрат і закінчуючи проектуванням протиобмерзачів і повітряних трубопроводів для всього експлуатаційного діапазону застосування літака. Наведено приклади використання розроблених наукових основ проектування при виконанні структурного аналізу мод

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26

Алексєєнко, Сергій вікторович, Сергей викторович Алексеенко та Serhei Vyktorovych Alekseyenko. "Науково-методологічні основи моделювання зледеніння аеродинамічних поверхонь літальних апаратів". Thesis, 2019. http://er.nau.edu.ua/handle/NAU/40503.

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Створено наукові та методологічні основи для розробки математичних моделей, методик, алгоритмів і програм, що описують процеси гідроаеродинаміки і тепломасопереносу, з урахуванням фазових переходів, що відбуваються при зледенінні літальних апаратів. Проведена серія експериментальних досліджень процесу замерзання вологи, що випадає на обтічну поверхню, яка включає вивчення мікрофізики процесу взаємодії переохолоджених крапель води з поверхнею, структури криги, що утворюється на поверхні, а також процесу замерзання переохолодженої поверхневої краплі. На основі проведених експериментів вд

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27

Hsieh, Yu-Shu, and 謝育樹. "Predictions of Ice Accretion on airfoils and Airfoil Aerodynamic Performance Degradation Due to Icing." Thesis, 2003. http://ndltd.ncl.edu.tw/handle/94376099265720767890.

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碩士<br>國立成功大學<br>航空太空工程學系碩博士班<br>91<br>In this study, a numerical method is developed to simulate the two—dimonsional shape of airfoil after icing, and to compute the airfoil aerodynamic lift coefficient degrading due to icing. The numerical analysis of ice accretion simulation is divided into four parts：(1) The calculation of low-speed flowfield by using turbulent Reynolds Averaged Navier-Stokes equations solver to obtain the phenomenon of flowfield over NACA-0012 section. (2) The results of the water droplet trajectories by the equation of motion in the flowfield as obtained in part 1 determi

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28

Jacob, Joel. "Experimental and computational aerodynamic analysis of ice fragments shed from aircraft surfaces." Thesis, 2006. http://hdl.handle.net/10057/573.

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Icing can pose problems due to both accretions on aircraft aerodynamic surfaces as well as through shedding of large ice particles from aircraft surfaces. The shed ice causes damage by impacting downstream aerodynamic surfaces and on ingestion by aft mounted engines. Present ice trajectory simulation tools have limited capabilities due to the lack of experimental aerodynamic force and moment data for ice fragments and the large number of variables that can affect the trajectories of ice particles in the aircraft flowfield like the particle shape, size, mass, initial velocity, particle shedding

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29

Standingford, David William Fin. "Optimal lifting surfaces, including end plates, ground effect & thickness / David William Fin Standingford." Thesis, 1997. http://hdl.handle.net/2440/19063.

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Bibliography: leaves 164-172.<br>xii, 172 leaves : ill. (some col.) ; 30 cm.<br>The task of calculating the aerodynamic load distribution on a thin three-dimensional lifting surface or wing of finite aspect ratio at small angle of attack presents difficulties for most numerical methods. The two-dimensional lifting-surface integral equation that must be solved is highly singular, and does not possess analytic solutions, even for simple plan-form geometries such as rectangles or ellipses.<br>Thesis (Ph.D.)--University of Adelaide, Dept. of Applied Mathematics, 1998

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30

Safaee, Alireza. "Nanostructured metal surfaces and their passivation for superhydrophobic and anti-icing applications = Les surfaces nanostructurées et leur passivation pour des applications des revêtements superhydrophobes et glaciophobes." Thèse, 2008. http://constellation.uqac.ca/169/1/030112159.pdf.

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Plusieurs systèmes et infrastructures stratégiques sont affectés ou cessent de fonctionner pendant les périodes hivernales accompagnées de givrage atmosphérique. Une des méthodes couramment utilisées pour diminuer les charges de glace ou de neige est l'utilisation des produits chimiques pour abaisser le point de congélation. Cependant, ces produits doivent être appliqués pendant le givrage ou juste avant l'accumulation de la glace, ce qui est difficile en pratique. De plus, ces produits sont nocifs pour l'environnement. C'est ainsi que de nouvelles méthodes, plus efficaces et moins nocives, so

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