ライブラリ登録: Guest
International Journal of Fluid Mechanics Research

年間 6 号発行

ISSN 印刷: 2152-5102

ISSN オンライン: 2152-5110

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 1.1 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 1.3 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.0002 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.33 SJR: 0.256 SNIP: 0.49 CiteScore™:: 2.4 H-Index: 23

Indexed in

NUMERICAL INVESTIGATION OF THE INFLUENCE OF HORN ICE FORMATION ON AIRFOILS AERODYNAMIC PERFORMANCES

巻 46, 発行 6, 2019, pp. 499-508
DOI: 10.1615/InterJFluidMechRes.2019026024
Get accessGet access

要約

The numerical studies of the aerodynamic characteristics of the wing profile NACA 0012 with horn ice formations are presented. The results have been compared with the experimental data obtained within low-velocity wind tunnel AT-4 "KHAI." Both shape and roughness of the outgrowths corresponded to icing regimes typical for glaze ice formation. The studies were carried out within a wide range of attack angle α = −4°... 18° when the Reynolds number was Re = 0.67 × 106 and flow velocity was V = 53 m/s. Effect of a flow-field structure on aerodynamic characteristics of the profile has been determined.

参考
  1. Alekseyenko, S.V., Numerical Simulation of the Icing Surfaces of the Cylinder and Profile, PAMM 2013, vol. 13, no. 1, pp. 299- 300,2013a.

  2. Alekseyenko, S.V. and Prykhodko, O.A., Numerical Simulation of Icing of a Cylinder and an Airfoil: Model Review and Computational Results, TsAGISci. J, vol. 44, no. 6, pp. 761-805,2013b.

  3. Alekseenko, S.V. and Prikhod'ko, A.A., Mathematical Modeling of Ice Body Formation on the Wing Airfoil Surface, Fluid Dy nam., vol. 49, no. 6, pp. 715-732,2014. DOI: 10.1134/S0015462814060039.

  4. Alekseenko, S.V., Mendig, C., Schulz, M., Sinapius, M., and Prykhodko, O.A., An Experimental Study of Freezing of Supercooled Water Droplet on Solid Surface, Tech. Phys. Lett., vol. 42, no. 5, pp. 524-527,2016. DOI: 10.1134/S1063785016050187.

  5. Alekseyenko, S., Sinapius, M., Schulz, M., and Prykhodko, O., Interaction of Supercooled Large Droplets with Aerodynamic Profile, SAE Tech. Paper 2015-01-2118,p. 12,2015. DOI: 10.4271/2015-01-2118.

  6. Aupoix, B. and Spalart, P.R., Extensions of the Spalart-Allmaras Turbulence Model to Account for Wall Roughness, Int. J. Heat Fluid Flow, vol. 24, pp. 454-462,2003.

  7. Deych, M.E. andFilippov, G.A., Gas Dynamics of Two-Phase Media, Moscow: ENERGIIA, 1968 (in Russian).

  8. Fortin, G., Ilinca, A., and Brandi, V., A New Roughness Computation Method and Geometric Accretion Model for Airfoil Icing, J. Aircraft, vol. 41, no. 1, pp. 119-127,2004.

  9. Fortin, G., Laforte, J., and Beisswenger, A., Prediction of Ice Shapes on NACA0012 2D Airfoil, Anti-Icing Mat. Int. Lab, FAA In-Flight Icing/Ground De-Icing Int. Conf. Exhib, SAE Tech. Paper 2003-01-2154,2003.

  10. Gent, R., TRAJICE2-A Combined Water Droplet Trajectory and Ice Accretion Prediction Program for Aerofoils, Royal Aerospace Establishment, Farnborough, U.K., Tech. Rep. 90054,1990.

  11. Guffond, D. and Brunet, L., Validation du Programme Bidimensionnel de Capitation, Oce National D'Etudes et deRecherches Chatillon, Cedex, France, Tech. Rep. RP 20/5146 SY, 1988.

  12. Louchez, P., Fortin, G., Mingione, G., and Brandi, V., Beads and Rivulets Modelling in Ice Accretion on a Wing, Am. Instit. Aeronautics Astronautics, 36th Aerospace Sci. Meeting Exhibit, Reno, Nevada, 1998.

  13. Mingione, G. and Brandi, V., Ice Accretion Prediction on Multielement Airfoils, J. Aircraft, vol. 35, no. 2, pp. 240-246,1998.

  14. Nigmatulin, R.I., Dynamics of Multiphase Media, Bocan Raton, FL: CRC Press, 1987 (in Russian).

  15. Prikhod'ko, A.A. and Alekseenko, S.V., Numerical Simulation of the Processes of Icing on Airfoils with Formation of a "Barrier" Ice, J. Eng. Phys. Thermophys., vol. 87, no. 3, pp. 598-607,2014. DOI: 10.1007/s10891-014-1050-0.

  16. Prykhodko, A.A. and Alekseenko, S.V., Numerical Simulation of the Process of Airfoil Icing in the Presence of Large Supercooled Water Drops, Tech. Phys. Lett., vol. 40, no. 10, pp. 884-887,2014. DOI: 10.1134/S1063785014100125.

  17. Rahmatulin, H.A., Fundamentals of Gas Dynamics of Interpenetrating Motions of Compressible Media, pp. 184-195, 1956 (in Russian).

  18. Roe, P.L., Characteristic-Based Schemes for the Euler Equations, Ann. Rev. FluidMech, vol. 18, no. 1, pp. 337-365,1986.

  19. Sedov, L.I., Continuum Mechanics, Moscow, Russia: Nauka, 1983 (in Russian).

  20. Spalart, P.R. and Allmaras, S.R., A One-Equation Turbulence Model for Aerodynamic Flow, AIAA Paper no. 92, p. 0439,1992.

  21. Tran, P., Brahimi, M.T., Paraschivoiu, I., Pueyo, A., and Tezok, F., Ice Accretion on Aircraft Wings with Thermodynamic Effects, Am. Instil Aeronautics. Astronautics, 32nd Aerospace Sci. Meeting Exhibit, Reno, Nevada, AIAA-1994-0605, p. 9, January 1994.

  22. Wright, W.B., User Manual for the Improved NASA Lewis Ice Accretion Code LEWICE 1.6, National Aeronautics and Space Administration, Cont. Rep. 198355, May 1995.

  23. Wright, W.B. and Rutkowski, A., Validation Results for LEWICE 2.0, NASA Tech. Rep. NASA/CR-1999-208690,1999.

950 記事の閲覧数 14 記事のダウンロード 記事の統計
950 記事の閲覧数 14 記事のダウンロード Google
Scholar
引用数

類似内容の記事:

INFLUENCE OF HIGH-BYPASS-RATIO TURBOFAN JETS ON AERODYNAMIC CHARACTERISTICS OF HIGH-LIFT WING TsAGI Science Journal, Vol.46, 2015, issue 7
Vladimir Fedorovich Tretyakov, Albert Vasilievich Petrov
STUDY OF VISCOUS−INVISCID INTERACTION ON AN OSCILLATING MODEL OF AN AIRPLANE WITH A SWEPT WING TsAGI Science Journal, Vol.40, 2009, issue 5
Vladimir Georgievich Markov, Tamara Ivanovna Trifonova, Ivan Vasilyevich Kolin, Viktor Konstantinovich Svyatodukh, Dmitry Valeryevich Shukhovtsov
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION TsAGI Science Journal, Vol.44, 2013, issue 1
Iraida Fedorovna Chelysheva, Sergey Valer'evich Chernov, Vladimir L'vovich Yumashev, Alexander Petrovich Kosykh, Sergey Mikhailovich Zadonsky, Garry Grantovich Nersesov
Comparison between SST and k-ε Models for the Computation of 3-D Flow past Isolated NACA Blade Profiles ICHMT DIGITAL LIBRARY ONLINE, Vol.10, 2006, issue
Djamel Cherrarred, Said Benmansour, E. G. Filali, Rabah Dizene, B. Noura
GAS-DYNAMIC FEATURES OF THE FLOW FIELD OVER A MODEL OF AN INTEGRATED HYPERSONIC FLYING VEHICLE TsAGI Science Journal, Vol.43, 2012, issue 1
Iraida Fedorovna Chelysheva, Sergey Valer'evich Chernov, Vladimir L'vovich Yumashev, Alexander Petrovich Kosykh, Sergey Mikhailovich Zadonsky, Garry Grantovich Nersesov
Begell Digital Portal Begellデジタルライブラリー 電子書籍 ジャーナル 参考文献と会報 リサーチ集 価格及び購読のポリシー Begell House 連絡先 Language English 中文 Русский Português German French Spain