THE ELEVATOR PARAMETERS STUDY OF JOINED WING CONFIGURATION IN TERM OF LIFT-TO-DRAG RATIO LOSSES DUE TO TRIMMING
DOI:
https://doi.org/10.18372/1990-5548.61.14222Keywords:
joined wing, box wing, elevator, longitudinal trimming, unmanned aerial vehicle, automationAbstract
The paper deals with estimation procedure of Lift-to-Drag ratio losses due to longitudinal trimming for several Joined Wing configuration in wide range of lift coefficient. A software for automated calculation of aerodynamic characteristics has been developed, that permit to explore an influence of elevator parameters (elevator span, position and wing configuration) on trimming characteristics of aircraft. The results of calculation for different layouts of Joined Wing are presented, by which it can be concluded that in some combination of the elevator parameters Lift-to-Drag ratio losses take negative values, hence, overall aerodynamic performance of trimmed configuration are better than for wing with zero elevator deflection. The usage of a developed software and proposed methodology make possible rapid evaluation of control surface parameters in wide range of parameters at early design stage.
References
J. Wolkovitch, “The Joined Wing Aircraft: an Overview,” Journal of Aircraft, vol. 23, no 3, pp. 161–178, 1986.
L. Prandtl, “Induced drag of multiplanes,” NACA, Washington, NACA Technical Note 182, Feb. 01, 1924.
New Ideas Sharpen Focus for Greener Aircraft | NASA. – [Electronic resource]. – Acces mode: https://www.nasa.gov/topics/aeronautics/features/greener_aircraft.html
A. Dane, “Diamond Eyes,” in Popular Mechanics, September 1993, pp. 30–33, 1993.
Innocon Micro Falcon. – [Electronic resource]. – Acces mode: http://www.innoconltd.com/? CategoryID=179&ArticleID=104
In Russia, are developing a new UAV "Frigate". – [Electronic resource]. – Acces mode: https://defence-blog.com/new/in-russia-are-developing-a-new-uav-frigate.html, 2015
Guizhou Soar Dragon. – [Electronic resource]. – Acces mode: https://en.wikipedia.org/wiki/ Guizhou_Soar_Dragon
C. Galinski, J. Hajduk, M. Kalinowski, M. Wichulski, and L. Stefanec, “Inverted joined wing scaled demonstrator programme,” in 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
A. Frediani, M. Gasperini, G. Saporito, and A.Rimondi, “Development of a PrandtlPlane aircraft configuration,” in XVII Congresso Nazionale AIDAA, Roma, vol. 4, pp. 2263–2276, 2003.
K.O. Predachenko, “Possibility of application joined wing layout for UAV,” in Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2015 IEEE International Conference, 2015, pp. 37–40.
K.O. Predachenko and O.L. Lemko, “Lift-to-Drag Ratio Losses due to Longitudinal Trimming in Joined Wing Configuration at Cruise Flight Mode,” in Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2017 IEEE International Conference, 2017, pp. 44–48.
Yu. N. Sviridenko and Yu. L. Ineshyn, “An Application of Panel-Vortex Method with Symmetrization of Singularities for Airplane Flow Calculation with Account of Jet Influence,” in The works of TsAGI, vol. 2622, pp. 41–53, 1996.
Pansym tools. – [Electronic resource]. – Acces mode: https://github.com/thexhs/pansym_tools.
Downloads
How to Cite
Issue
Section
License
The scientific journal “Electronics and control systems” adheres to the principles of Open Access and provides free, immediate, and permanent access to all published materials without financial, technical, or legal barriers for readers.
All articles are published in Open Access under the Creative Commons Attribution 4.0 International (CC BY 4.0) license.
Copyright
Authors who publish their works in the journal “Electronics and control systems”:
-
retain the copyright to their publications;
-
grant the journal the right of first publication of the article;
-
agree to the distribution of their materials under the CC BY 4.0 license;
-
have the right to reuse, archive, and distribute their works (including in institutional and subject repositories), provided that proper reference is made to the original publication in the journal.



