论文信息 - Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings - 字舞流文

Vibration and dynamic response control of elastically tailored nonuniform adaptive aircraft wings

Liviu Librescu | Sung Soo Na | S. Na | L. Librescu

[1] E. Smith,et al. Formulation and evaluation of an analytical model for composite box-beams , 1991 .

[2] L. Librescu,et al. Response of laminated composite flat panels to sonic boom and explosive blast loadings , 1990 .

[3] L. Librescu,et al. Integrated structural tailoring and control using adaptive materials for advanced aircraft wings , 1996 .

[4] Leonard Meirovitch,et al. Control of Cantilever Vibration via Structural Tailoring and Adaptive Materials , 1997 .

[5] Liviu Librescu,et al. Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour , 1993 .

[6] Ephrahim Garcia,et al. A Self-Sensing Piezoelectric Actuator for Collocated Control , 1992 .

[7] Min-Yung Chang. Active vibration control of composite structures , 1990 .

[8] Jann N. Yang,et al. New Optimal Control Algorithms for Structural Control , 1987 .

[9] Ohseop Song,et al. Adaptive vibrational behavior of cantilevered structures modeled as composite thin-walled beams , 1993 .