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COMPARISON OF HEXAGONAL, SQUARE AND CIRCULAR SECTIONED HONEYCOMB PERFORMANCE IN A WIND TUNNEL

Yıl 2021, Cilt: 6 Sayı: 2, 38 - 49, 31.10.2021

Öz

Experimental studies are very important in designing of a new product. In the aerodynamic designs, wind tunnel tests are commonly used in experimental studies. In the experimental studies accuracy is the most critical point to verify the results. Laminar flow is preferred at test section to obtain accurate results. Turbulence intensity is the main drawback of the wind tunnel tests. Hence in this study, turbulence intensity of the hexagonal, square and circular sectioned honeycomb is investigated. In the numerical studies, a circular sectioned subsonic wind tunnel is used. The computational fluid dynamic (CFD) analysis of three-dimensional (3D) flow in a circular sectioned desktop size wind tunnel is used for comparison.

Kaynakça

  • [1] Wang Y, Song Y, Yu J, Chen F. Effect of the injection orientation and position on the leakage flow in a honeycomb-tip turbine cascade. International Journal of Heat and Mass Transfer 2019; 144: 118633
  • [2] Wang Y, Yu J, Song Y, Chen F. Parameter optimization of the composite honeycomb tip in a türbine cascade. Energy 2020; 197: 117236
  • [3] Zaniewski D, Klimaszewski P, Klonowicz P, Lampart P, Witanowski Ł, Je˛drzejewski Ł, Suchocki T, Antczak Ł. Performance of the honeycomb type sealing’s in organic vapor micro turbines. Energy 2021; 226: 120242
  • [4] Wang Y, Song Y, Yu J, Chen F. Effect of cooling injection on the leakage flow of a turbine cascade with honeycomb tip. Applied Thermal Engineering 2018; 133: 690–703
  • [5] Massinia D, Facchinia B, Miciob M, Bianchinib C, Ceccherinic A, Innocenti L. Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance. Energy Procedia 2014; 45: 502 – 511
  • [6] Yi L, Changchuan X, Chao Y, Jialin C. Gust response analysis and wind tunnel test for a high-aspect ratio wing. Chinese Journal of Aeronautics 2016; 29(1): 91–103
  • [7] Koreanschi A, Gabor O S, Acotto J, Brianchon G, Portier G, Botez R M, Mamou M, Mebarki Y. Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests. Chinese Journal of Aeronautics 2017; 30(1): 164–174
  • [8] Joe M, Kammegne T, Botez R M, Grigorie L T, Mamou M, Mebarki Y. Proportional fuzzy feed-forward architecture control validation by wind tunnel tests of a morphing wing. Chinese Journal of Aeronautics 2017; 30(2): 561–576
  • [9] Zhang W, Sun J, Wang L, Wu J, He L. Rotor airfoil aerodynamic design method and wind tunnel test verification. Chinese Journal of Aeronautics 2020; 33(8): 2123–2132
  • [10] Meng Y, Wan Z, Xie C *, An C. Time-domain nonlinear aeroelastic analysis and wind tunnel test of a flexible wing using strain-based beam formulation. Chinese Journal of Aeronautics 2021; 34(1): 380–396
  • [11] Oliviu ¸ Gabora S, Koreanschia A, Boteza R M, Mamoub M, Mebarki Y. Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance. Aerospace Science and Technology 2016; 53: 136–153
  • [12] Xua J, Fub Z, Baib J, Zhangc Y, Duand Z, Zhang Y. Study of boundary layer transition on supercritical natural laminar flow wing at high Reynolds number through wind tunnel experiment. Aerospace Science and Technology 2018; 80: 221–231
  • [13] He S, Guo S, Liu Y, Luo W. Passive gust alleviation of a flying-wing aircraft by analysis and wind-tunnel test of a scaled model in dynamic similarity. Aerospace Science and Technology 2021; 113: 106689
  • [14] Göv, I., Mehmet Hanifi Dogru, and Umit Korkmaz. "Improvement of the aerodynamic performance of NACA 4412 using the adjustable airfoil profile during the flight." Journal of The Faculty of Engineering and Architecture of Gazi University 34.2 (2019): 1110-1125.
  • [15] Doğru, Mehmet Hanifi. "Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles." Çukurova University Journal of the Faculty of Engineering and Architecture 32.3 (2017): 39-46.
  • [16] İ̇brahim, GÖV., and Mehmet Hanifi DOĞRU. "AERODYNAMIC OPTIMIZATION OF NACA 0012 AIRFOIL." The International Journal of Energy and Engineering Sciences 5.2 (2020): 146-155.
  • [17] Korkmaz, Ümit, GÖV. İ̇brahim, and Mehmet Hanifi DOĞRU. "AERODYNAMIC ANALYSES OF NACA 63-215." The International Journal of Energy and Engineering Sciences 5.2 (2020): 156-166.
  • [18] Eyercioglu O, Gov K, Aksoy A. Abrasive Flow Machining of Asymmetric Spur Gear Forging Die. Harran University Journal of Engineering 2019; 4(1): 12-20.
  • [19] Göv K. Experimental investigation of the effects of the coolant on the performance parameters of electrical discharge drilling of some aerospace materials. Journal of the Faculty of Engineering and Architecture of Gazi University 2017; 32:1, 293-301.
  • [20] Göv K, Soydan O, Eyercioğlu Ö. Improving the surface quality of Ti-6Al-4V alloy produced by electrical discharge machining with abrasive flow machining. Journal of the Faculty of Engineering and Architecture of Gazi University 2020; 35:3 1159-1170.
Yıl 2021, Cilt: 6 Sayı: 2, 38 - 49, 31.10.2021

Öz

Kaynakça

  • [1] Wang Y, Song Y, Yu J, Chen F. Effect of the injection orientation and position on the leakage flow in a honeycomb-tip turbine cascade. International Journal of Heat and Mass Transfer 2019; 144: 118633
  • [2] Wang Y, Yu J, Song Y, Chen F. Parameter optimization of the composite honeycomb tip in a türbine cascade. Energy 2020; 197: 117236
  • [3] Zaniewski D, Klimaszewski P, Klonowicz P, Lampart P, Witanowski Ł, Je˛drzejewski Ł, Suchocki T, Antczak Ł. Performance of the honeycomb type sealing’s in organic vapor micro turbines. Energy 2021; 226: 120242
  • [4] Wang Y, Song Y, Yu J, Chen F. Effect of cooling injection on the leakage flow of a turbine cascade with honeycomb tip. Applied Thermal Engineering 2018; 133: 690–703
  • [5] Massinia D, Facchinia B, Miciob M, Bianchinib C, Ceccherinic A, Innocenti L. Analysis of flat plate honeycomb seals aerodynamic losses: effects of clearance. Energy Procedia 2014; 45: 502 – 511
  • [6] Yi L, Changchuan X, Chao Y, Jialin C. Gust response analysis and wind tunnel test for a high-aspect ratio wing. Chinese Journal of Aeronautics 2016; 29(1): 91–103
  • [7] Koreanschi A, Gabor O S, Acotto J, Brianchon G, Portier G, Botez R M, Mamou M, Mebarki Y. Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speeds, Part II - Experimental validation using Infra-Red transition measurement from Wind Tunnel tests. Chinese Journal of Aeronautics 2017; 30(1): 164–174
  • [8] Joe M, Kammegne T, Botez R M, Grigorie L T, Mamou M, Mebarki Y. Proportional fuzzy feed-forward architecture control validation by wind tunnel tests of a morphing wing. Chinese Journal of Aeronautics 2017; 30(2): 561–576
  • [9] Zhang W, Sun J, Wang L, Wu J, He L. Rotor airfoil aerodynamic design method and wind tunnel test verification. Chinese Journal of Aeronautics 2020; 33(8): 2123–2132
  • [10] Meng Y, Wan Z, Xie C *, An C. Time-domain nonlinear aeroelastic analysis and wind tunnel test of a flexible wing using strain-based beam formulation. Chinese Journal of Aeronautics 2021; 34(1): 380–396
  • [11] Oliviu ¸ Gabora S, Koreanschia A, Boteza R M, Mamoub M, Mebarki Y. Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance. Aerospace Science and Technology 2016; 53: 136–153
  • [12] Xua J, Fub Z, Baib J, Zhangc Y, Duand Z, Zhang Y. Study of boundary layer transition on supercritical natural laminar flow wing at high Reynolds number through wind tunnel experiment. Aerospace Science and Technology 2018; 80: 221–231
  • [13] He S, Guo S, Liu Y, Luo W. Passive gust alleviation of a flying-wing aircraft by analysis and wind-tunnel test of a scaled model in dynamic similarity. Aerospace Science and Technology 2021; 113: 106689
  • [14] Göv, I., Mehmet Hanifi Dogru, and Umit Korkmaz. "Improvement of the aerodynamic performance of NACA 4412 using the adjustable airfoil profile during the flight." Journal of The Faculty of Engineering and Architecture of Gazi University 34.2 (2019): 1110-1125.
  • [15] Doğru, Mehmet Hanifi. "Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles." Çukurova University Journal of the Faculty of Engineering and Architecture 32.3 (2017): 39-46.
  • [16] İ̇brahim, GÖV., and Mehmet Hanifi DOĞRU. "AERODYNAMIC OPTIMIZATION OF NACA 0012 AIRFOIL." The International Journal of Energy and Engineering Sciences 5.2 (2020): 146-155.
  • [17] Korkmaz, Ümit, GÖV. İ̇brahim, and Mehmet Hanifi DOĞRU. "AERODYNAMIC ANALYSES OF NACA 63-215." The International Journal of Energy and Engineering Sciences 5.2 (2020): 156-166.
  • [18] Eyercioglu O, Gov K, Aksoy A. Abrasive Flow Machining of Asymmetric Spur Gear Forging Die. Harran University Journal of Engineering 2019; 4(1): 12-20.
  • [19] Göv K. Experimental investigation of the effects of the coolant on the performance parameters of electrical discharge drilling of some aerospace materials. Journal of the Faculty of Engineering and Architecture of Gazi University 2017; 32:1, 293-301.
  • [20] Göv K, Soydan O, Eyercioğlu Ö. Improving the surface quality of Ti-6Al-4V alloy produced by electrical discharge machining with abrasive flow machining. Journal of the Faculty of Engineering and Architecture of Gazi University 2020; 35:3 1159-1170.
Toplam 20 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Bölüm Research Article
Yazarlar

İbrahim Göv 0000-0002-5513-0158

Yayımlanma Tarihi 31 Ekim 2021
Kabul Tarihi 17 Kasım 2021
Yayımlandığı Sayı Yıl 2021 Cilt: 6 Sayı: 2

Kaynak Göster

APA Göv, İ. (2021). COMPARISON OF HEXAGONAL, SQUARE AND CIRCULAR SECTIONED HONEYCOMB PERFORMANCE IN A WIND TUNNEL. The International Journal of Energy and Engineering Sciences, 6(2), 38-49.

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