共 50 条
- [1] Direct aeroelastic bifurcation analysis of a symmetric wing based on Euler equations JOURNAL OF AIRCRAFT, 2005, 42 (03): : 731 - 737
- [2] Aeroelastic analysis method of wings based on Euler equations Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2002, 20 (02): : 257 - 261
- [3] AEROELASTIC ANALYSIS OF WINGS USING THE EULER EQUATIONS WITH A DEFORMING MESH JOURNAL OF AIRCRAFT, 1991, 28 (11): : 781 - 788
- [4] Aeroelastic analysis of wings using the Euler equations with a deforming mesh Robinson, Brian A., 1600, (28):
- [5] Energy-based aeroelastic analysis of a morphing wing MODELING, SIGNAL PROCESSING, AND CONTROL FOR SMART STRUCTURES 2007, 2007, 6523
- [7] Aeroelastic calculations for the Hawk aircraft using the Euler equations JOURNAL OF AIRCRAFT, 2005, 42 (04): : 1005 - 1012
- [8] Euler-based dynamic aeroelastic analysis of shell structures JOURNAL OF AIRCRAFT, 2000, 37 (05): : 840 - 845
- [9] Stochastic Nonlinear Aeroelastic Analysis of a Swept Wing Based on Nastran ADVANCES IN COMPUTATIONAL MODELING AND SIMULATION, PTS 1 AND 2, 2014, 444-445 : 738 - +
- [10] Direct solution of the aeroelastic stability equations Bismarck-Nasr, Maher N., 1600, AIAA, Washington, DC, United States (31):