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Hermann schlichting and the boundary-layer theory. 2-The effect of undulating leadingedge modifications on NACA 0021 airfoil characteristics. 3-Bird or bat: comparing airframe design and flight performance. 4-Drag reduction in nature. 5-Hydrodynamic design of the humpback whale flipper. 6-Reduction of bluff-body drag and suppression of vortex shedding by the introduction of wavy separation lines. 7-Experimental evaluation of sinusoidal leading edges. 8-Effects of leading-edge protuberances on airfoil performance. 9-Numerical study of passive and active flow separation control over a NACA0012 airfoil. 10-Control of the separated flow around an airfoil using a wavy leading edge inspired by humpback whale flippers. 11-Flow over a wing with leading-edge undulations. 12-Vortex shedding and aerodynamic performance of airfoil with multiscale trailing-edge modifications. 13-Wind tunnel testing of a novel wingsuit design. 14-The effect of surface materials and morphology on wingsuit aerodynamics. 15-Towards a combined CAD and CFD development process of a wingsuit. 16-A preliminary anthropometry standard for Australian Army equipment evaluation. 17-Theory of wing sections: including a summary of airfoil data. 18-Aircraft design: A systems engineering approach. 19-CFD Modeling of a Wingsuit. 20-3D Design and Simulation Methods for the Development of Wingsuits. 21-The effect of undulating leading-edge modifications on NACA 0021 airfoil characteristics.