Citation: | Pan Deng, Wu Zhigang, Yang Chaoet al. Flight loads analysis of flexible aircraft under large deformations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(10): 1158-1161. (in Chinese) |
[1] Drela M.Method for simultaneous wing aerodynamic and structural load prediction [J].Journal of Aircraft,1990,27(8):692-699 [2] Drela M.Integrated simulation model for preliminary aerodynamic structural,and control-law design of aircraft .AIAA-99-24752,1999 [3] Langford J.The daedalus project: a summary of lessons learned .AIAA-89-2048,1989 [4] Rodden W P,Johnson E H.MSC/Nastran aeroelastic analysis user-s guide V68 [M].Los Angeles: MSC Software Coporation,1994:35-65 [5] Mingguet P.Static and dynamic behavior of composite helicopter rotor blades under large deflections .MA,USA:Departent of Aeronautics and Astronaatics,Massachusetts Institute of Technology,1989 [6] Katz J,Plotkin A.Low-speed aerodynamics [M].Cambridge: Cambridge University Press,2001:331-360
|