Evaluation of a Potential Flow Model for Propeller and Wind Turbine Design
AIAA 2006-1305 The Effect of IGV Wake Impingement on a Rotor Boundary Layer
CRS Study Results for Myopia and Astigmatism Using the Nidek Laser
Design of a High-Lift, Thick Airfoil for Unmanned Aerial Vehicle Applications
Application of computational methods to the aerodynamic development of a prototype race car
Performance analysis of 2D-barcode-enhanced documents [2422-34]
Cellular Structures in the Flow over the Flap of a Two-Element Wing
Experimental Characterization of a Supersonic Flow Control Actuator (AIAA 2006-0478)
One Beam Two View Holographic Particle Image Velocimetry System
Application of Leading-Edge Vortex Manipulations to Reduce Wing Rock Amplitudes