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/sl/article/optimization-of-the-dynamic-balance-of-an-aileron/>. Date accessed: 20 dec. 2024. 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/sl/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
%A Mesarič, Mihael %A Kosel, Franc %D 2002 %T Optimization of the Dynamic Balance of an Aileron %B 2002 %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/sl/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. 20 Dec. 2024
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/sl/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/sl/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/sl/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)
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.