Aeroelastic Analysis of Wind Tunnel Test Data of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap (VCCTEF)
暂无分享,去创建一个
[1] Eric Ting,et al. Static Aeroelastic and Longitudinal Trim Model of Flexible Wing Aircraft Using Finite-Element Vortex-Lattice Coupled Solution , 2014 .
[2] Eric Ting,et al. 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 , 2013 .
[3] Sonia Lebofsky,et al. Experimental Investigation of a Flexible Wing with a Variable Camber Continuous Trailing Edge Flap Design , 2014 .
[4] Michael J. Aftosmis,et al. Static Aeroelastic Analysis with an Inviscid Cartesian Method , 2014 .
[5] Dewey H. Hodges,et al. Introduction to Structural Dynamics and Aeroelasticity: Contents , 2002 .
[6] Nhan Nguyen,et al. Elastically Shaped Wing Optimization and Aircraft Concept for Improved Cruise Efficiency , 2013 .
[7] Eric Ting,et al. A Mission-Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift-to-Drag Ratios of Future N+3 Transport Aircraft , 2013 .
[8] J. Anderson,et al. Fundamentals of Aerodynamics , 1984 .
[9] Eli Livne,et al. The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration , 2015 .