AERODYNAMIC ANALYSIS OF A RC AIRPLANE

Volume: 2 Number: 1 January 1, 2017
  • İbrahim Göv
The International Journal of Energy and Engineering Sciences Cover
The International Journal of Energy and Engineering Sciences
PDF Download
EN

AERODYNAMIC ANALYSIS OF A RC AIRPLANE

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

Keywords

References

  1. Adiwibowo B., (2013). Retrieved from https://grabcad.com/library/cessna-172-- 1.
  2. AirfoilTools, (2017). Retrieved from http://airfoiltools.com/airfoil/details?airfoil=naca2412-il.
  3. Atmeh G.M., Hasan Z., Darwish F., 2010. Design and stress analysis of a general aviation aircraft wing. COMSOL Conference, Boston.
  4. 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.
  5. 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.
  6. Doğru, M. H., Güzelbey İ. H., (2014). Kanal Fanının İtme Kuvvetinin Deneysel Olarak Hesaplanması. Makina tasarım ve imalat dergisi, 14(1).
  7. 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.
  8. Hedges, L. S., Travin, A. K., Spalart, P. R., (2002). Detached-Eddy Simulations over a Simplified Landing Gear. Journal of Fluids Engineering, 124.

Details

Primary Language

English

Subjects

-

Journal Section

-

Authors

İbrahim Göv This is me

Publication Date

January 1, 2017

Submission Date

-

Acceptance Date

-

Published in Issue

Year 2017 Volume: 2 Number: 1

IZ

https://izlik.org/JA23HN59JJ

Cite

RIS / Bibtex
APA
Göv, İ. (2017). AERODYNAMIC ANALYSIS OF A RC AIRPLANE. The International Journal of Energy and Engineering Sciences, 2(1), 31-40. https://izlik.org/JA23HN59JJ
AMA
1.Göv İ. AERODYNAMIC ANALYSIS OF A RC AIRPLANE. IJEES. 2017;2(1):31-40. https://izlik.org/JA23HN59JJ
Chicago
Göv, İbrahim. 2017. “AERODYNAMIC ANALYSIS OF A RC AIRPLANE”. The International Journal of Energy and Engineering Sciences 2 (1): 31-40. https://izlik.org/JA23HN59JJ.
EndNote
Göv İ (January 1, 2017) AERODYNAMIC ANALYSIS OF A RC AIRPLANE. The International Journal of Energy and Engineering Sciences 2 1 31–40.
IEEE
[1]İ. Göv, “AERODYNAMIC ANALYSIS OF A RC AIRPLANE”, IJEES, vol. 2, no. 1, pp. 31–40, Jan. 2017, [Online]. Available: https://izlik.org/JA23HN59JJ
ISNAD
Göv, İbrahim. “AERODYNAMIC ANALYSIS OF A RC AIRPLANE”. The International Journal of Energy and Engineering Sciences 2/1 (January 1, 2017): 31-40. https://izlik.org/JA23HN59JJ.
JAMA
1.Göv İ. AERODYNAMIC ANALYSIS OF A RC AIRPLANE. IJEES. 2017;2:31–40.
MLA
Göv, İbrahim. “AERODYNAMIC ANALYSIS OF A RC AIRPLANE”. The International Journal of Energy and Engineering Sciences, vol. 2, no. 1, Jan. 2017, pp. 31-40, https://izlik.org/JA23HN59JJ.
Vancouver
1.İbrahim Göv. AERODYNAMIC ANALYSIS OF A RC AIRPLANE. IJEES [Internet]. 2017 Jan. 1;2(1):31-40. Available from: https://izlik.org/JA23HN59JJ

IMPORTANT NOTES

No part of the material protected by this copyright may be reproduced or utilized in any form or by any means, without the prior written permission of the copyright owners, unless the use is a fair dealing for the purpose of private study, research or review. The authors reserve the right that their material can be used for purely educational and research purposes. All the authors are responsible for the originality and plagiarism, multiple publication, disclosure and conflicts of interest and fundamental errors in the published works.

*Please note that  All the authors are responsible for the originality and plagiarism, multiple publication, disclosure and conflicts of interest and fundamental errors in the published works. Author(s) submitting a manuscript for publication in IJEES also accept that the manuscript may go through screening for plagiarism check using IThenticate software. For experimental works involving animals, approvals from relevant ethics committee should have been obtained beforehand assuring that the experiment was conducted according to relevant national or international guidelines on care and use of laboratory animals.  Authors may be requested to provide evidence to this end.
 
**Authors are highly recommended to obey the IJEES policies regarding copyrights/Licensing and ethics before submitting their manuscripts.


Copyright © 2026. AA. All rights reserved