Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Eduardas Lasauskas"'
Publikováno v:
Mokslas: Lietuvos Ateitis, Vol 1, Iss 6 (2011)
Thermal localization and their strongest zone centering by artificial neural networks (ANN), and it are used by the automatic or semiautomatic control system of unmanned aerial vehicles (UAV). Artificial neural network take input data from aircraf
Externí odkaz:
https://doaj.org/article/5d13ecd149de48e4be04861b598da085
Publikováno v:
Mokslas: Lietuvos Ateitis, Vol 1, Iss 6 (2011)
The transition location on the FX 66-S-196 V1 wing section was analyzed with the using interactive program XFOIL of Mark Drela, MIT. Calculated results of transition location were compared with published measurement data from a wind tunnel at Delft U
Externí odkaz:
https://doaj.org/article/5c5b088d34114c5ba473c61c8e368aab
Autor:
Paulius Gildutis, Eduardas Lasauskas
Publikováno v:
Mokslas: Lietuvos Ateitis, Vol 1, Iss 6 (2011)
A computer-based geometrical model of the Lak-17a sailplane was generated with the program AVL (Athena Vortex Lattice), which is designed to analyse the characteristics of flight and to provide a rapid analysis of the configuration of an aircraft. Va
Externí odkaz:
https://doaj.org/article/84521585e9364130a53ded5b1f2aebd5
Publikováno v:
Aviation, Vol 13, Iss 1 (2009)
Three wing sections FX66‐S‐196VI, E603 and AH82–150A were analyzed. Measured data of these wing sections are published. First wing section was measured in Stuttgart University and in Delft University of Technology, when other two wing sections
Externí odkaz:
https://doaj.org/article/3a666879ae4b4f33917ac41c67f79718
Publikováno v:
Aviation, Vol 11, Iss 4 (2007)
A comparison of predicted and measured aerodynamic characteristics of the original NACA 23012 airfoil and an airfoil with a trailing edge tab is presented. XFOIL code is used for prediction. It is shown that the modification of the airfoils only on t
Externí odkaz:
https://doaj.org/article/35c1ea2b3d13492abfeff5742e8b4cbb
Autor:
Eduardas Lasauskas
Publikováno v:
Aviation, Vol 9, Iss 3 (2005)
A comparison of predicted and measured laminar‐turbulent transition on the airfoil is presented. The MSES code is used for a prediction. The experimental data are taken from an experiment of W. Würz. Comparison of calculated results with measured
Externí odkaz:
https://doaj.org/article/4f7b678f028248b68c48e25baac2787e
Publikováno v:
Aviation, Vol 9, Iss 1 (2005)
Calculation results for 11 different finite span wings are presented. Calculations were made by a combination of a numerical solution of lifting line theory with a technique developed to evaluate nonlinear section lift data. Aerodynamic coefficients
Externí odkaz:
https://doaj.org/article/2a90d996d5a142bfbed274c9b2c3cd08
Autor:
Eduardas Lasauskas, Paulius Gildutis
Publikováno v:
Mokslas - Lietuvos ateitis. 1:106-110
A computer-based geometrical model of the Lak-17a sailplane was generated with the program AVL (Athena Vortex Lattice), which is designed to analyse the characteristics of flight and to provide a rapid analysis of the configuration of an aircraft. Va
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b44ce0d98cf7ef6fca3d8a8ef0794aa3
https://doi.org/10.3846/mla.2009.6.22
https://doi.org/10.3846/mla.2009.6.22
Publikováno v:
Mokslas - Lietuvos ateitis. 1:129-132
Thermal localization and their strongest zone centering by artificial neural networks (ANN), and it are used by the automatic or semiautomatic control system of unmanned aerial vehicles (UAV). Artificial neural network take input data from aircraft a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c83a1b3b45d0124ba9fddf173df2318d
https://doi.org/10.3846/mla.2009.6.27
https://doi.org/10.3846/mla.2009.6.27
Publikováno v:
Mokslas - Lietuvos ateitis. 1:120-124
The transition location on the FX 66‑S‑196 V1 wing section was analyzed with the using interactive program XFOIL of Mark Drela, MIT. Calculated results of transition location were compared with published measurement data from a wind tunnel at Del
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ac0bc15569667f64b529f00ebb9e3d1c
https://doi.org/10.3846/mla.2009.6.25
https://doi.org/10.3846/mla.2009.6.25