Advances in Aerospace Engineering

Research Article

A Computational Investigation of Unsteady Aerodynamics of Insect-Inspired Fixed Wing Micro Aerial Vehicle’s 2D Airfoil

Figure 13

Contours of pressure efficient −10° through +15° of AOA.
504049.fig.0013a
(a) −10° AOA
504049.fig.0013b
(b) −5° AOA
504049.fig.0013c
(c) 0° AOA
504049.fig.0013d
(d) 5° AOA
504049.fig.0013e
(e) 10° AOA
504049.fig.0013f
(f) 15° AOA