AIAA-2009-382-170[1]
Aerodynamics Course Notes v3
Lesson 6 - Lift Continued - Theory of Flight
1 Flexible flaps for separation control on a wing with low aspect ratio Dipl. Ing. G. Patone Dr. W. Müller Dr. R. Bannasch Prof. Dr. Ing. I. Rechenberg.
Optimization of Aerodynamic Efficiency for Morphing MAV Wing
Pullin Jfm2004
Aeroelasticity text-Chapter 2.pdf
Terrestial Locomotion Requires a balance between (1) displacement, (2) robustness, (3) energy and (4) stability. All four are usually in opposition: Improving.
HELICOPTER AERODYNAMICS