The integrated design of maneuver processes and flight loads was investigated for modern fighters. The aeroelastic correction of fight loads and maneuver processes, and maneuver load alleviation were further studied. It indicates that the influences of structural deformation on elastic aerodynamic loads and maneuver processes are significant, and the maneuver loads can be availably alleviated using modern control technique. The investigation of this work can be applied in analysis and study on the maneuver processes and flight loads for the modern fighters.
���÷ɻ�ǿ�Ⱥնȹ淶��ί��.���÷ɻ�ǿ�Ⱥնȹ淶:�����غ�[M].����:������ҵ������,1992:3-4 Editor committee of military aircraft strength and stiffness specification.Military aircraft strength and stiffness specification[M].Beijing:National Defence Industrial Press,1992:3-4(in Chinese)
Hodges D H,Pierce G A.Introduction to structural dynamics and aeroelasticity[M].Cambridge:Cambridge University Press,2001
Platanitis G,Strganac T W.Suppression of control reversal using leading and trailing-edge control surfaces[J].Journal of Guidance,Control,and Dynamics.2005,28(3):452-460
Dowell E H,Bliss D B,Clark R L.Aeroelastic wing with leading and trailing edge control surfaces[J].Journal of Aircraft.2003,40(3):559-565
������,��־��,�.���Էɻ����������Ӧ���غɿ���[J].�ɻ�����,2010(4):40-44 Zhu Yangzhen,Wu Zhigang,Yang Chao.Longitudinal maneuver response and loads control of aeroelastic airplanes[J].Aircraft Engineering,2010(4):40-44 (in Chinese)