[American Institute of Aeronautics and Astronautics AIAA Atmospheric Flight Mechanics (AFM) Conference - Boston, MA ()] AIAA Atmospheric Flight Mechanics (AFM) Conference - Coupled Vortex-Lattice Flight Dynamic Model with Aeroelastic Finite-Element Model of Flexible Wing Transport Aircraft with Variable Camber Continuous Trailing Edge Flap for Drag Reduction
Nguyen, Nhan T., Ting, Eric B., Nguyen, Daniel, Dao, Tung, Trinh, KhanhYear:
2013
Language:
english
DOI:
10.2514/6.2013-4746
File:
PDF, 1.31 MB
english, 2013