Historical perspective on analysis and control of aeroelastic responses

被引:108
作者
Mukhopadhyay, V [1 ]
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
关键词
D O I
10.2514/2.5108
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A historical perspective on analysis and control of aeroelastic responses was presented. Research works in the multidisciplinary field of aeroelastic analysis, involving solid mechanics, fluid dynamics, and control theory are also reviewed. The developments in nonlinear aeroservoelasticity (ASE) include nonlinear aeroelastic response identification, limit-cycle of nonlinear aeroelastic systems, and wavelet filtering for ASE robustness estimation.
引用
收藏
页码:673 / 684
页数:12
相关论文
共 162 条
[1]  
ABEL I, 1988, P 16 C INT COUNC AER
[2]  
ABEL I, 1980, 2010 NASA TP
[3]   A DOUBLET-LATTICE METHOD FOR CALCULATING LIFT DISTRIBUTIONS ON OSCILLATING SURFACES IN SUBSONIC FLOWS [J].
ALBANO, E ;
RODDEN, WP .
AIAA JOURNAL, 1969, 7 (02) :279-&
[4]  
ANDERSON JD, 1997, HIST AERODYNAMICS, V8, P14
[5]  
[Anonymous], 2018, Mathematical Theory of Optimal Processes
[6]  
APPA K, 2000, AFRLVAWPTR20003033
[7]   PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J].
ASHLEY, H ;
ZARTARIAN, G .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12) :1109-1118
[8]  
ASHLEY H, 1986, APPL MECH UPDATE, P117
[9]  
ASHLEY H, 1981, 811738 AIAA
[10]  
ASHLEY H, 1970, APPL MECH REV, V23, P119