kaz29Вестник Казахстанско-Британского технического университетаHerald of the Kazakh-British Technical University1998-66882959-8109Казахстанско-Британский Технический Университет10.55452/1998-6688-2021-18-2-20-25kaz29-78Research ArticleФИЗИКО-МАТЕМАТИЧЕСКИЕ И ТЕХНИЧЕСКИЕ НАУКИPHYSICAL, MATHEMATICAL AND TECHNICAL SCIENCESУСЛОВИЯ ВОЗНИКНОВЕНИЯ ОБЛЕДЕНЕНИЙ НА АЭРОДИНАМИЧЕСКИХ ПРОФИЛЯХ И МЕТОДИКИ ИХ РАСЧЕТАCONDITIONS FOR THE OCCURRENCE OF ICING ON AERODYNAMIC PROFILES AND METHODS OF THEIR CALCULATIONhttps://orcid.org/0000-0002-0903-3517АхажановС. Б.AkhazhanovS. B.

Akhazhanov Sungat Berkinovich – PhD, Associate Professor of the Department of Algebra, Mathematical Logic and Geometry named after prof. T.G. Mustafina

stjg@mail.ruhttps://orcid.org/0000-0002-9454-904XСкоробогатовС. В.SkorobogatovS. V.

Skorobogatov Sergey Vladimirovich - 2nd year undergraduate student of the Department of Algebra, Mathematical Logic and Geometry named after prof. T.G. Mustafina

skoroboga1ov@gmail.comКарагандинский университет имени академика Е.А. БукетоваКазахстанBuketov Karaganda universityKazakhstan2021041120211822025Copyright © Ахажанов С.Б., Скоробогатов С.В., 20212021Ахажанов С.Б., Скоробогатов С.В.Akhazhanov S.B., Skorobogatov S.V.Данная работа распространяется под лицензией Creative Commons Attribution 4.0.This work is licensed under a Creative Commons Attribution 4.0 License.https://vestnik.kbtu.edu.kz/jour/article/view/78

В данной статье произведен анализ методов и моделей, подходящих для исследования обледенения аэродинамической поверхности (крыла). Рассмотрены системы по противодействию обледенительному эффекту. Изучены методики и рассмотрены модели расчета образований льда на аэродинамических поверхностях. Дальнейшее направление для изучения эффекта обледенения будет проведено при учете особенности обтекания тел вязкой сжимаемой средой с учетом несущей и жидкой фазы, в случае изменения геометрических параметров тел и учет этого изменения на внешний поток.

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.

условия обледененияпотоки около аэродинамической поверхностивлага на обтекаемой поверхностиобразования изморози или льдааэродинамических поверхностейicing conditionsflows near the aerodynamic surfacemoisture on the streamlined surfaceformation of frost or iceaerodynamic surfacesReferencesAircraft Icing Handbook [Electronic resource]. - Access mode: https://www.skybrary.aero/bookshelf/books/659.pdf. Date of treatment (11.12.2020).Aircraft Icing Handbook [Electronic resource]. - Access mode: https://www.skybrary.aero/bookshelf/books/659.pdf. Date of treatment (11.12.2020).I.H. Abbott, Von Doenhoff and A.E. Theory of Wing Section // Dover Publications, Inc. - 2014. - 302 p.I.H. Abbott, Von Doenhoff and A.E. Theory of Wing Section // Dover Publications, Inc. - 2014. - 302 p.W.B. Wright. Users Manual for Improved NASA Lewis Ice Accreation Code LEWICE (NASA) // Contractor report. - 2017. - 95 p.W.B. Wright. Users Manual for Improved NASA Lewis Ice Accreation Code LEWICE (NASA) // Contractor report. - 2017. - 95 p.S.F. Ackley, M.K. Templeton. Computer Modeling of Atmospheric Ice Accretion // CRREL REPORT 2. - 2015.- P. 15-35.S.F. Ackley, M.K. Templeton. Computer Modeling of Atmospheric Ice Accretion // CRREL REPORT 2. - 2015.- P. 15-35.G. Fortin. Prediction of ice shapes on NACA airfoil [Electronic resource]. - Access mode: https://www.researchgate.net/publication/228387958_Prediction_of_ice_shapes_on_NACA0012_2D_airfoil. Date of treatment (05.12.2020).G. Fortin. Prediction of ice shapes on NACA airfoil [Electronic resource]. - Access mode: https://www.researchgate.net/publication/228387958_Prediction_of_ice_shapes_on_NACA0012_2D_airfoil. Date of treatment (05.12.2020).T.P. Meshcheryakov. Designing a protection system for aircraft and helicopters // Moscow: Mechanical Engineering. – 2001. - 222 p.T.P. Meshcheryakov. Designing a protection system for aircraft and helicopters // Moscow: Mechanical Engineering. – 2001. - 222 p.J.D. Anderson. Computational Fluid Dynamics. The Basics with Applications // McGraw-Hill Education. - 2017. - P. 32-77.J.D. Anderson. Computational Fluid Dynamics. The Basics with Applications // McGraw-Hill Education. - 2017. - P. 32-77.Ice Accreation Simulation, Agard, [Electronic resource]. - Access mode: https://www.ftp.rta.nato.int/public/Agard9.pdf. Date of treatment (11/18/2020).Ice Accreation Simulation, Agard, [Electronic resource]. - Access mode: https://www.ftp.rta.nato.int/public/Agard9.pdf. Date of treatment (11/18/2020).C. Bak, P. Fuglsang. Airfoil Characteristics for Wind Turbines // Ris-R-1065 (EN). - Risø National Laboratory. - Roskilde. - 2011. - P. 63-90.C. Bak, P. Fuglsang. Airfoil Characteristics for Wind Turbines // Ris-R-1065 (EN). - Risø National Laboratory. - Roskilde. - 2011. - P. 63-90.L. Battisti. Class III - Basics on Icing For Wind Turbines // Lecture slides from course. - Wind Turbine Ice Prevention Systems Selection and Design. - Technical University of Denmark. - 2014L. Battisti. Class III - Basics on Icing For Wind Turbines // Lecture slides from course. - Wind Turbine Ice Prevention Systems Selection and Design. - Technical University of Denmark. - 2014J.J. Chung, H.E. Add. A Numerical Evaluation of Icing effects on a Natural Laminar Flow Airfoil // NASA TM. - 2016. - P. 12-18.J.J. Chung, H.E. Add. A Numerical Evaluation of Icing effects on a Natural Laminar Flow Airfoil // NASA TM. - 2016. - P. 12-18.

The authors declare that there are no conflicts of interest present.