Optimization of the Dynamic Balance of an Aileron

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MESARIČ, Mihael ;KOSEL, Franc .
Optimization of the Dynamic Balance of an Aileron. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 48, n.1, p. 41-48, july 2017. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/>. Date accessed: 26 jun. 2022. 
doi:http://dx.doi.org/.
Mesarič, M., & Kosel, F.
(2002).
Optimization of the Dynamic Balance of an Aileron.
Strojniški vestnik - Journal of Mechanical Engineering, 48(1), 41-48.
doi:http://dx.doi.org/
@article{.,
	author = {Mihael  Mesarič and Franc  Kosel},
	title = {Optimization of the Dynamic Balance of an Aileron},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {48},
	number = {1},
	year = {2002},
	keywords = {: aileron; dynamic balance; optimization methods; computer software; },
	abstract = {This paper deals with the use of the aileron balance criterion as one of the criteria for providing freedom from wing flutter on general-category airplanes. Based on this criterion and using the Pro/ENGINEER computer-aided-design software, the required mass of the balance weight was obtained. The results from the model were confirmed by our experiments. By using the gradient-optimisation method, the optimum size and position of the balance weight with respect to the minimisation of the aileron mass were achieved.},
	issn = {0039-2480},	pages = {41-48},	doi = {},
	url = {https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/}
}
Mesarič, M.,Kosel, F.
2002 July 48. Optimization of the Dynamic Balance of an Aileron. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 48:1
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%A Kosel, Franc 
%D 2002
%T Optimization of the Dynamic Balance of an Aileron
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%9 : aileron; dynamic balance; optimization methods; computer software; 
%! Optimization of the Dynamic Balance of an Aileron
%K : aileron; dynamic balance; optimization methods; computer software; 
%X This paper deals with the use of the aileron balance criterion as one of the criteria for providing freedom from wing flutter on general-category airplanes. Based on this criterion and using the Pro/ENGINEER computer-aided-design software, the required mass of the balance weight was obtained. The results from the model were confirmed by our experiments. By using the gradient-optimisation method, the optimum size and position of the balance weight with respect to the minimisation of the aileron mass were achieved.
%U https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/
%0 Journal Article
%R 
%& 41
%P 8
%J Strojniški vestnik - Journal of Mechanical Engineering
%V 48
%N 1
%@ 0039-2480
%8 2017-07-07
%7 2017-07-07
Mesarič, Mihael, & Franc  Kosel.
"Optimization of the Dynamic Balance of an Aileron." Strojniški vestnik - Journal of Mechanical Engineering [Online], 48.1 (2002): 41-48. Web.  26 Jun. 2022
TY  - JOUR
AU  - Mesarič, Mihael 
AU  - Kosel, Franc 
PY  - 2002
TI  - Optimization of the Dynamic Balance of an Aileron
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - : aileron; dynamic balance; optimization methods; computer software; 
N2  - This paper deals with the use of the aileron balance criterion as one of the criteria for providing freedom from wing flutter on general-category airplanes. Based on this criterion and using the Pro/ENGINEER computer-aided-design software, the required mass of the balance weight was obtained. The results from the model were confirmed by our experiments. By using the gradient-optimisation method, the optimum size and position of the balance weight with respect to the minimisation of the aileron mass were achieved.
UR  - https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/
@article{{}{.},
	author = {Mesarič, M., Kosel, F.},
	title = {Optimization of the Dynamic Balance of an Aileron},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {48},
	number = {1},
	year = {2002},
	doi = {},
	url = {https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/}
}
TY  - JOUR
AU  - Mesarič, Mihael 
AU  - Kosel, Franc 
PY  - 2017/07/07
TI  - Optimization of the Dynamic Balance of an Aileron
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 48, No 1 (2002): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - : aileron, dynamic balance, optimization methods, computer software, 
N2  - This paper deals with the use of the aileron balance criterion as one of the criteria for providing freedom from wing flutter on general-category airplanes. Based on this criterion and using the Pro/ENGINEER computer-aided-design software, the required mass of the balance weight was obtained. The results from the model were confirmed by our experiments. By using the gradient-optimisation method, the optimum size and position of the balance weight with respect to the minimisation of the aileron mass were achieved.
UR  - https://www.sv-jme.eu/article/optimization-of-the-dynamic-balance-of-an-aileron/
Mesarič, Mihael, AND Kosel, Franc.
"Optimization of the Dynamic Balance of an Aileron" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 48 Number 1 (07 July 2017)

Authors

Affiliations

  • University of Ljubljana, Faculty of Mechanical Engineering, Slovenia
  • University of Ljubljana, Faculty of Mechanical Engineering, Slovenia

Paper's information

Strojniški vestnik - Journal of Mechanical Engineering 48(2002)1, 41-48
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.

This paper deals with the use of the aileron balance criterion as one of the criteria for providing freedom from wing flutter on general-category airplanes. Based on this criterion and using the Pro/ENGINEER computer-aided-design software, the required mass of the balance weight was obtained. The results from the model were confirmed by our experiments. By using the gradient-optimisation method, the optimum size and position of the balance weight with respect to the minimisation of the aileron mass were achieved.

: aileron; dynamic balance; optimization methods; computer software;