AERODYNAMICS OF SMALL VEHICLES
By Thomas J. Mueller, J. Delaurier. 2003
516 citations recorded by the source corpus.
Subfields: Aerospace Engineering
View Paper: https://www.semanticscholar.org/paper/a1193f89df5ff26fb512cf3c3a022e3e1aa04c3f
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In Aerospace Engineering
Citations in the corpus
- Adaptive separation control of a laminar boundary layer using online dynamic mode decomposition (2020, background): “LSBs may develop on laminar airfoils (Joslin 1998), low-pressure turbine blades (Hodson & Howell 2005), small aerial vehicles (Mueller & DeLaurier 2003), and wind-turbine blades (Sorensen 2011) and, in nearly all cases, have a detrimental effect on performance.”
- On vortex shedding from an airfoil in low-Reynolds-number flows (2009, background): “Tani 1964; Carmichael 1981; Mueller & DeLaurier 2003 ).”
- The ultra-low Reynolds number airfoil wake (2010, background): “gained an increasing practical importance, with a variety of applications, such as micro air vehicles (MAVs), unmanned air vehicles (UAVs), small wind turbines, and lowspeed/high-altitude aircraft ( Mueller and DeLaurier 2003 ).”
- Aerodynamics of Low Reynolds Number Flyers (2007, background): “The tip vortex forms a low-pressure region on the top surface of the wing, which provides additional lift force (Mueller and DeLaurier, 2003).”