Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Enlai Sha"'
Publikováno v:
Actuators, Vol 10, Iss 7, p 142 (2021)
A static aeroelastic analysis of the flexible trailing edge is conducted to calculate the deformed shape, aerodynamic coefficients and corresponding driving pressure. A physical flexible trailing edge model is manufactured using a honeycomb structure
Externí odkaz:
https://doaj.org/article/5ed0a038b45a4535aa18628885617d97
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:888-899
Purpose This paper aims to assess the aeroacoustic and aerodynamic performance of a morphing airfoil with a flexible trailing edge (FTE). The objective is to make a comparison of the aerodynamic noise characteristics between the conventional airfoil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a839d3c34c33214fb1d22c1c2a9c2e3c
https://doi.org/10.1108/aeat-11-2020-0263
https://doi.org/10.1108/aeat-11-2020-0263
Publikováno v:
International Conference on Mechanical Design and Simulation (MDS 2022).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab7ffbdb3c5832d6dee8d78c9df318ce
https://doi.org/10.1117/12.2638900
https://doi.org/10.1117/12.2638900
Publikováno v:
Aircraft Engineering and Aerospace Technology. 91:1-9
Purpose The purpose of this paper is to investigate the unsteady aerodynamic characteristics in the deflection process of a morphing wing with flexible trailing edge, which is based on time-accurate solutions. The dynamic effect of deflection process
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed4faeefba2662d2e32fc078300c1c35
https://doi.org/10.1108/aeat-04-2017-0101
https://doi.org/10.1108/aeat-04-2017-0101
Publikováno v:
Actuators, Vol 10, Iss 142, p 142 (2021)
Actuators
Volume 10
Issue 7
Actuators
Volume 10
Issue 7
A static aeroelastic analysis of the flexible trailing edge is conducted to calculate the deformed shape, aerodynamic coefficients and corresponding driving pressure. A physical flexible trailing edge model is manufactured using a honeycomb structure
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7e33f793c444284c29c1d604af300e03
https://doi.org/10.3390/act10070142
https://doi.org/10.3390/act10070142