IN THIS PROJECT THE ASYMMETRIC CASE WILL BE STUDIED. FURTHER THE EFFECTS OF AN ASYMMETRIC BLI WILL BE MODELED VIA CFD TO QUANTIFY THE ENHANCED PROPULSION EFFICIENCY AND DRAG REDUCTION FOR VARIOUS AIRFRAME GEOMETRIES.
$145,972FY2020National Aeronautics and Space AdministrationNASA
University Of California Irvine, Irvine CA