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Year 2017, Volume 2, Issue 1, 31 - 40, 01.01.2017

Abstract

References

  • Adiwibowo B., (2013). Retrieved from https://grabcad.com/library/cessna-172-- 1.
  • AirfoilTools, (2017). Retrieved from http://airfoiltools.com/airfoil/details?airfoil=naca2412-il.
  • Atmeh G.M., Hasan Z., Darwish F., 2010. Design and stress analysis of a general aviation aircraft wing. COMSOL Conference, Boston.
  • Chitte P., Jadhav P.K., Bansode S.S., 2013. Statistic and dynamic analysis of typical wing structure of aircraft using Nastran. International Journal of Application or Innovation in Engineering & Management (IJAIEM) 2, 7.
  • Doğru M.H., (2017). Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles. Çukurova University Journal of the Faculty of Engineering and Architecture, In Press.
  • Doğru, M. H., Güzelbey İ. H., (2014). Kanal Fanının İtme Kuvvetinin Deneysel Olarak Hesaplanması. Makina tasarım ve imalat dergisi, 14(1).
  • Doğru, M. H., İ. H. Güzelbey, and Göv İ., (2016). Ducted Fan Effect on the Elevation of a Concept Helicopter When the Ducted Faintail Is Located in a Ground Effect Region. Journal of Aerospace Engineering, DOI: 10.1061/(ASCE)AS.1943-5525.0000519.
  • Hedges, L. S., Travin, A. K., Spalart, P. R., (2002). Detached-Eddy Simulations over a Simplified Landing Gear. Journal of Fluids Engineering, 124.
  • Imrana, M.,Shabbir, A.R.M, Haneefe M., (2015). FE Analysis for Landing Gear of Test Air Craft. Materials Today: Proceedings, 2, 2170 – 2178.

AERODYNAMIC ANALYSIS OF A RC AIRPLANE

Year 2017, Volume 2, Issue 1, 31 - 40, 01.01.2017

Abstract

In this study, lift force and drag force of a RC airplane was calculated using computational fluid dynamic (CFD) analysis. NACA 2412 airfoil was used for wing design. When the aircraft is moving into the air, it subjects to aerodynamic forces. These aerodynamic forces are the drag, lift, and thrust forces. Drag force produces a resistant to relative motion. Lift is the force that directly opposes the weight of an airplane and holds the airplane in the air. Thrust is generated by the engines of the aircraft through some kind of propulsion system. Drag and lift forces were investigated at maximum speed to represent the aerodynamic performance of a RC airplane

References

  • Adiwibowo B., (2013). Retrieved from https://grabcad.com/library/cessna-172-- 1.
  • AirfoilTools, (2017). Retrieved from http://airfoiltools.com/airfoil/details?airfoil=naca2412-il.
  • Atmeh G.M., Hasan Z., Darwish F., 2010. Design and stress analysis of a general aviation aircraft wing. COMSOL Conference, Boston.
  • Chitte P., Jadhav P.K., Bansode S.S., 2013. Statistic and dynamic analysis of typical wing structure of aircraft using Nastran. International Journal of Application or Innovation in Engineering & Management (IJAIEM) 2, 7.
  • Doğru M.H., (2017). Investigation of Velocity Distribution and Turbulent Energy for the Different Tip Shaped Projectiles. Çukurova University Journal of the Faculty of Engineering and Architecture, In Press.
  • Doğru, M. H., Güzelbey İ. H., (2014). Kanal Fanının İtme Kuvvetinin Deneysel Olarak Hesaplanması. Makina tasarım ve imalat dergisi, 14(1).
  • Doğru, M. H., İ. H. Güzelbey, and Göv İ., (2016). Ducted Fan Effect on the Elevation of a Concept Helicopter When the Ducted Faintail Is Located in a Ground Effect Region. Journal of Aerospace Engineering, DOI: 10.1061/(ASCE)AS.1943-5525.0000519.
  • Hedges, L. S., Travin, A. K., Spalart, P. R., (2002). Detached-Eddy Simulations over a Simplified Landing Gear. Journal of Fluids Engineering, 124.
  • Imrana, M.,Shabbir, A.R.M, Haneefe M., (2015). FE Analysis for Landing Gear of Test Air Craft. Materials Today: Proceedings, 2, 2170 – 2178.

Details

Primary Language English
Journal Section Research Article
Authors

İbrahim GÖV This is me

Publication Date January 1, 2017
Published in Issue Year 2017, Volume 2, Issue 1

Cite

Bibtex @ { ijees612273, journal = {The International Journal of Energy and Engineering Sciences}, issn = {2602-294X}, address = {Gaziantep üniversitesi Mühendislik Fakültesi Dekanlığı}, publisher = {Gaziantep University}, year = {2017}, volume = {2}, pages = {31 - 40}, doi = {}, title = {AERODYNAMIC ANALYSIS OF A RC AIRPLANE}, key = {cite}, author = {Göv, İbrahim} }
APA Göv, İ. (2017). AERODYNAMIC ANALYSIS OF A RC AIRPLANE . The International Journal of Energy and Engineering Sciences , 2 (1) , 31-40 . Retrieved from https://dergipark.org.tr/en/pub/ijees/issue/48358/612273
MLA Göv, İ. "AERODYNAMIC ANALYSIS OF A RC AIRPLANE" . The International Journal of Energy and Engineering Sciences 2 (2017 ): 31-40 <https://dergipark.org.tr/en/pub/ijees/issue/48358/612273>
Chicago Göv, İ. "AERODYNAMIC ANALYSIS OF A RC AIRPLANE". The International Journal of Energy and Engineering Sciences 2 (2017 ): 31-40
RIS TY - JOUR T1 - AERODYNAMIC ANALYSIS OF A RC AIRPLANE AU - İbrahim Göv Y1 - 2017 PY - 2017 N1 - DO - T2 - The International Journal of Energy and Engineering Sciences JF - Journal JO - JOR SP - 31 EP - 40 VL - 2 IS - 1 SN - 2602-294X- M3 - UR - Y2 - 2021 ER -
EndNote %0 The International Journal of Energy and Engineering Sciences AERODYNAMIC ANALYSIS OF A RC AIRPLANE %A İbrahim Göv %T AERODYNAMIC ANALYSIS OF A RC AIRPLANE %D 2017 %J The International Journal of Energy and Engineering Sciences %P 2602-294X- %V 2 %N 1 %R %U
ISNAD Göv, İbrahim . "AERODYNAMIC ANALYSIS OF A RC AIRPLANE". The International Journal of Energy and Engineering Sciences 2 / 1 (January 2017): 31-40 .
AMA Göv İ. AERODYNAMIC ANALYSIS OF A RC AIRPLANE. IJEES. 2017; 2(1): 31-40.
Vancouver Göv İ. AERODYNAMIC ANALYSIS OF A RC AIRPLANE. The International Journal of Energy and Engineering Sciences. 2017; 2(1): 31-40.
IEEE İ. Göv , "AERODYNAMIC ANALYSIS OF A RC AIRPLANE", The International Journal of Energy and Engineering Sciences, vol. 2, no. 1, pp. 31-40, Jan. 2017

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