AERODYNAMICS OF SMALL VEHICLES
作者： Thomas J. Mueller , James D. DeLaurier
DOI: 10.1146/ANNUREV.FLUID.35.101101.161102
关键词: Aerodynamics 、 Propulsion 、 Computer science 、 Aeroelasticity 、 Reynolds number 、 Aerospace engineering 、 Flow separation 、 Separation (aeronautics) 、 Airfoil 、 Laminar flow
摘要: ▪ Abstract In this review we describe the aerodynamic problems that must be addressed in order to design a successful small aerial vehicle. The effects of Reynolds number and aspect ratio (AR) on performance fixed-wing vehicles are described. boundary-layer behavior airfoils is especially important flight regime. results experimental studies, including influence laminar separation bubbles, discussed. Several examples unmanned (UAVs) regime Also, brief survey analytical models for oscillating flapping-wing propulsion presented. These range from earliest where quasi-steady, attached flow assumed, those account unsteady shed vortex wake as well aeroelastic flapping wing. Experiments complemented analysis led ornithopter also
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