Araştırma Makalesi
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Dört Rotorlu İHA Pervanesinde Uçuş Hızı ve Dönme Hızının İtme Katsayısı Üzerine Etkilerinin Sayısal Araştırılması

Yıl 2021, , 9 - 15, 30.06.2021
https://doi.org/10.30518/jav.872627

Öz

Bu çalışmada, dört rotorlu bir İHA pervanesi üzerinde uçuş hızı ve dönme hızının pervanelerin aerodinamik performansı açısından büyük önem arz eden itme katsayısına olan etkilerini incelemek amacıyla sayısal araştırma gerçekleştirilmiştir. Bu amaçla 11-inç çapında bir pervane üzerinde dik uçuş koşulları altında farklı uçuş hızları ve dönüş hızlarında hesaplamalı akışkanlar dinamiği analizleri gerçekleştirilmiştir. Hesaplamalarda kullanılacak optimum ağ elemanı sayısını belirlemek için aynı zamanda ağdan bağımsızlık çalışması da gerçekleştirilmiştir. Sonuç olarak, k-ω SST türbülans modeli ile gerçekleştirilen analiz sonuçları, dönüş hızındaki artışın daha yüksek türbülans kinetik enerjisine sebep olduğunu göstermiştir. Ayrıca, yine dönüş hızındaki artışın deneysel sonuçlarla sayısal tahminlerin arasındaki farkı artırdığı, fakat uçuş hızından ise daha bağımsız hale getirdiği görülmüştür.

Kaynakça

  • O. Kose and T. Oktay, “Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions,” European Journal of Science and Technology, 15, 132-142, 2019.
  • T. Oktay and Y. Eraslan, “Computational Fluid Dynamics (CFD) Investigation of a Quadrotor UAV Propeller” International Conference on Energy, Environment and Storage of Energy, 21-25, 2020.
  • Y. Eraslan, E. Özen and T. Oktay, “A Literature Review on Determination of Quadrotor Unmanned Aerial Vehicles Propeller Thrust and Power Coefficients” EJONS 10th International Conference on Mathematics, Engineering, Natural & Medical Sciences, 108-118, 2020.
  • D. Shukla, N. Hiremath, S. Patel and N. Komerath, “Aerodynamic Interactions Study on Low-Re Coaxial and Quad-rotor Configurations” ASME International Mechanical Engineering Congress and Exposition, 58424, 2017.
  • R. W. Deters, “Reynolds number effects on the performance of small-scale propellers” 32nd AIAA Applied Aerodynamics Conference, 2014.
  • P. Burgers, “A Thrust Equation Treats Propellers and Rotors as Aerodynamic Cycles and Calculates Their Thrust Without Resorting to the Blade Element Method” International Journal of Aviation Aeronautics, and Aerospace, 6(5), 2019.
  • A. Şumnu, İ. H. Güzelbey and O. Öğücü, “Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm” International Journal of Aerospace Engineering, 2020.
  • S. Yener and M. Perçin, “Numerical Investigation of Propeller-Frame Arm Interaction in Hovering Flight” Journal of Aeronautics and Space Technologies, 13(2), 189-200, 2020.
  • H. A. Kutty and P. Rajendran, “3D CFD Simulation and Experimental Validation of Small APC Slow Flyer Propeller Blade” Aerospace, 4(1), 10, 2017.
  • S. P. Yeong and S. S. Dol, “Aerodynamic Optimization of Micro Aerial Vehicle” Journal of Applied Fluid Mechanics, 9(5), 2016.
  • J. F. Céspedes and O. D. Lopez, “Simulation and Validation of the Aerodynamic Performance of a Quadcopter in Hover Condition Using Overset Mesh” AIAA Aviation 2019 Forum, 2019.
  • E. Kuantama and R. Tarca, “Correction of Wind Effect on Quadcopter” International Conference on Sustainable Information Engineering and Technology (SIET), 257-261, 2018.
  • J. Brandt and M. Selig, “Propeller Performance Data at Low Reynolds Numbers” 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011.
  • T. Oktay and Y. Eraslan, “Mesh Independence Study on Computational Fluid Dynamics (CFD) Analysis of A Quad-Rotor UAV Propeller” 3rd International European Conference on Interdisciplinary Scientific Researches, 495-501, 2021.
  • T. Oktay and Y. Eraslan, “Evaluation of Various Turbulence Models in Computational Fluid Dynamics (CFD) Investigation of a Quad-rotor UAV Propeller” 3rd International European Conference on Interdisciplinary Scientific Researches, 502-509, 2021.
  • H. Yao and H. Zhang, “A Simple Method for Estimating Transition Locations on Blade Surface of Model Propellers to be Used for Calculating Viscous Force” International Journal of Naval Architecture and Ocean Engineering, 10(4), 477-490, 2018.

Numerical Investigation of Effects of Airspeed and Rotational Speed on Quadrotor UAV Propeller Thrust Coefficient

Yıl 2021, , 9 - 15, 30.06.2021
https://doi.org/10.30518/jav.872627

Öz

In this article, a numerical investigation was performed on a quadrotor UAV propeller with the aim of examining effects of airspeed and rotational speed on thrust coefficient, which is one of the most important parameters on propeller aerodynamic performance. In that purpose, Computational Fluid Dynamics (CFD) analyses of an 11-inch propeller were carried out at different airspeeds and rotational speeds in vertical climbing flight condition. In order to have optimum number of mesh elements in computational domain, mesh independence analyses were also conducted. In conclusion, results of the analyses with k-ω SST turbulence model were shown that, increase in rotational speed was leaded to higher turbulent kinetic energy. Furthermore, higher rotational speeds also resulted in higher differences between numerical estimations and experimental data, but found to become more independent from airspeed.

Kaynakça

  • O. Kose and T. Oktay, “Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions,” European Journal of Science and Technology, 15, 132-142, 2019.
  • T. Oktay and Y. Eraslan, “Computational Fluid Dynamics (CFD) Investigation of a Quadrotor UAV Propeller” International Conference on Energy, Environment and Storage of Energy, 21-25, 2020.
  • Y. Eraslan, E. Özen and T. Oktay, “A Literature Review on Determination of Quadrotor Unmanned Aerial Vehicles Propeller Thrust and Power Coefficients” EJONS 10th International Conference on Mathematics, Engineering, Natural & Medical Sciences, 108-118, 2020.
  • D. Shukla, N. Hiremath, S. Patel and N. Komerath, “Aerodynamic Interactions Study on Low-Re Coaxial and Quad-rotor Configurations” ASME International Mechanical Engineering Congress and Exposition, 58424, 2017.
  • R. W. Deters, “Reynolds number effects on the performance of small-scale propellers” 32nd AIAA Applied Aerodynamics Conference, 2014.
  • P. Burgers, “A Thrust Equation Treats Propellers and Rotors as Aerodynamic Cycles and Calculates Their Thrust Without Resorting to the Blade Element Method” International Journal of Aviation Aeronautics, and Aerospace, 6(5), 2019.
  • A. Şumnu, İ. H. Güzelbey and O. Öğücü, “Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm” International Journal of Aerospace Engineering, 2020.
  • S. Yener and M. Perçin, “Numerical Investigation of Propeller-Frame Arm Interaction in Hovering Flight” Journal of Aeronautics and Space Technologies, 13(2), 189-200, 2020.
  • H. A. Kutty and P. Rajendran, “3D CFD Simulation and Experimental Validation of Small APC Slow Flyer Propeller Blade” Aerospace, 4(1), 10, 2017.
  • S. P. Yeong and S. S. Dol, “Aerodynamic Optimization of Micro Aerial Vehicle” Journal of Applied Fluid Mechanics, 9(5), 2016.
  • J. F. Céspedes and O. D. Lopez, “Simulation and Validation of the Aerodynamic Performance of a Quadcopter in Hover Condition Using Overset Mesh” AIAA Aviation 2019 Forum, 2019.
  • E. Kuantama and R. Tarca, “Correction of Wind Effect on Quadcopter” International Conference on Sustainable Information Engineering and Technology (SIET), 257-261, 2018.
  • J. Brandt and M. Selig, “Propeller Performance Data at Low Reynolds Numbers” 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011.
  • T. Oktay and Y. Eraslan, “Mesh Independence Study on Computational Fluid Dynamics (CFD) Analysis of A Quad-Rotor UAV Propeller” 3rd International European Conference on Interdisciplinary Scientific Researches, 495-501, 2021.
  • T. Oktay and Y. Eraslan, “Evaluation of Various Turbulence Models in Computational Fluid Dynamics (CFD) Investigation of a Quad-rotor UAV Propeller” 3rd International European Conference on Interdisciplinary Scientific Researches, 502-509, 2021.
  • H. Yao and H. Zhang, “A Simple Method for Estimating Transition Locations on Blade Surface of Model Propellers to be Used for Calculating Viscous Force” International Journal of Naval Architecture and Ocean Engineering, 10(4), 477-490, 2018.
Toplam 16 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Uzay Mühendisliği
Bölüm Araştırma Makaleleri
Yazarlar

Tuğrul Oktay 0000-0003-4860-2230

Yüksel Eraslan 0000-0002-5158-5171

Yayımlanma Tarihi 30 Haziran 2021
Gönderilme Tarihi 1 Şubat 2021
Kabul Tarihi 28 Haziran 2021
Yayımlandığı Sayı Yıl 2021

Kaynak Göster

APA Oktay, T., & Eraslan, Y. (2021). Numerical Investigation of Effects of Airspeed and Rotational Speed on Quadrotor UAV Propeller Thrust Coefficient. Journal of Aviation, 5(1), 9-15. https://doi.org/10.30518/jav.872627

Journal of Aviation - JAV 


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