TY - GEN
T1 - Influence of Kinematics on Aerodynamic Characteristics of an Albatross-Like Flexible Flapping Wing in Forward Flight
AU - Gao, Nongyue
AU - Xie, Changchuan
AU - Yang, Chao
N1 - Publisher Copyright:
© The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2024.
PY - 2024
Y1 - 2024
N2 - Flapping wings have attracted much attention in recent years due to various merits. Many efforts have been made to study the kinematics and flexibility of flapping wings. However, the kinematics of flapping wing with bionic geometric shape and structural flexibility are still lacking in comprehensive exploration. In this paper, the aerodynamic characteristics and dynamic response of an albatross-like flapping wing undergoing different kinds of kinematics have been numerically explored. The results revealed the assocaition among flapping degree, pitching degree, phase difference, force coefficients and displacement response. Enlarging the flapping amplitude is beneficial to lift coefficient increasement, and introducing pitching is advantageous to drag coefficient declination. Compared with no phase difference between pitching and flapping, pitching phase lead can moderate lift coefficient changes in a smaller range with a good effect on retaining thrust, while phase lag may amplify that range at the cost of the drastically increasement of drag coefficient. The results provided a reference for the kinematic design of bird-like flapping wings from the perspectives of aerodynamic characteristics and dynamic response, and proposed a feasible method for the numerical simulation and analysis of bionic flexible flapping wings based on fluid-structure interaction.
AB - Flapping wings have attracted much attention in recent years due to various merits. Many efforts have been made to study the kinematics and flexibility of flapping wings. However, the kinematics of flapping wing with bionic geometric shape and structural flexibility are still lacking in comprehensive exploration. In this paper, the aerodynamic characteristics and dynamic response of an albatross-like flapping wing undergoing different kinds of kinematics have been numerically explored. The results revealed the assocaition among flapping degree, pitching degree, phase difference, force coefficients and displacement response. Enlarging the flapping amplitude is beneficial to lift coefficient increasement, and introducing pitching is advantageous to drag coefficient declination. Compared with no phase difference between pitching and flapping, pitching phase lead can moderate lift coefficient changes in a smaller range with a good effect on retaining thrust, while phase lag may amplify that range at the cost of the drastically increasement of drag coefficient. The results provided a reference for the kinematic design of bird-like flapping wings from the perspectives of aerodynamic characteristics and dynamic response, and proposed a feasible method for the numerical simulation and analysis of bionic flexible flapping wings based on fluid-structure interaction.
KW - Aerodynamic characteristics
KW - Flapping wing
KW - Kinematics
KW - Phase difference
KW - Structural flexibility
UR - https://www.scopus.com/pages/publications/85200205699
U2 - 10.1007/978-981-97-3998-1_102
DO - 10.1007/978-981-97-3998-1_102
M3 - 会议稿件
AN - SCOPUS:85200205699
SN - 9789819739974
T3 - Lecture Notes in Electrical Engineering
SP - 1312
EP - 1323
BT - 2023 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2023, Proceedings - Volume I
A2 - Fu, Song
PB - Springer Science and Business Media Deutschland GmbH
T2 - Asia-Pacific International Symposium on Aerospace Technology, APISAT 2023
Y2 - 16 October 2023 through 18 October 2023
ER -