TY - JOUR
T1 - Review and prospect of flutter boundary prediction methods for flight flutter testing
AU - Zhang, Weiwei
AU - Zhong, Huashou
AU - Xiao, Hua
AU - Ye, Zhengyin
N1 - Publisher Copyright:
©, 2015, AAAS Press of Chinese Society of Aeronautics and Astronautics. All right
PY - 2015/5/25
Y1 - 2015/5/25
N2 - Flight flutter testing, whose objective is to identify the flutter boundary, is an indispensible course for new aircraft to finalize. Because of the extremely great risk, high consumption and long period, researchers have been always pursuing a more secure, accurate and efficient flutter boundary prediction method. Based on the summary and analysis of the previous research, from the aspects of conventional flutter boundary prediction methods and new methods for flight flutter testing, this paper makes a more comprehensive and relatively concise introduction of many kinds of flutter prediction methods, and it highlights the basic principles, merits and demerits as well as the development of these methods. According to the fundamental principles and characteristics of various methods, they are divided into two categories, namely, introducing stability parameters methods and considering a coupled fluid-structure system method. Then, the two kinds of methods are compared and summarized. Finally, technical difficulties encountered at present and the development trend in the field of flight flutter testing are preliminary discussed.
AB - Flight flutter testing, whose objective is to identify the flutter boundary, is an indispensible course for new aircraft to finalize. Because of the extremely great risk, high consumption and long period, researchers have been always pursuing a more secure, accurate and efficient flutter boundary prediction method. Based on the summary and analysis of the previous research, from the aspects of conventional flutter boundary prediction methods and new methods for flight flutter testing, this paper makes a more comprehensive and relatively concise introduction of many kinds of flutter prediction methods, and it highlights the basic principles, merits and demerits as well as the development of these methods. According to the fundamental principles and characteristics of various methods, they are divided into two categories, namely, introducing stability parameters methods and considering a coupled fluid-structure system method. Then, the two kinds of methods are compared and summarized. Finally, technical difficulties encountered at present and the development trend in the field of flight flutter testing are preliminary discussed.
KW - Aeroelasticity
KW - Basic principles
KW - Flight flutter testing
KW - Flutter boundary prediction
KW - Technical difficulties
UR - http://www.scopus.com/inward/record.url?scp=84930749775&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2015.0036
DO - 10.7527/S1000-6893.2015.0036
M3 - 文献综述
AN - SCOPUS:84930749775
SN - 1000-6893
VL - 36
SP - 1367
EP - 1384
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 5
ER -