Nonlinear Lift on a Triangular Airfoil in Low-Reynolds-Number Compressible Flow

Numerical and experimental analyses of the aerodynamic performance of a triangular airfoil in low-Reynolds-number compressible flow are performed. This airfoil is one of the candidates for propeller blades on a possible future Martian air vehicle design. Based on past experimental studies conducted...

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Veröffentlicht in:	Journal of aircraft 2015-05, Vol.52 (3), p.924-931
Hauptverfasser:	Munday, Phillip M, Taira, Kunihiko, Suwa, Tetsuya, Numata, Daiju, Asai, Keisuke
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace engineering Aircraft Airfoils Angle of attack Atmosphere Boundary conditions Compressible flow Computational fluid dynamics Direct numerical simulation Elongated structure Engineering schools Fluid dynamics Fluid flow Incompressible flow Lift Low Reynolds number flow Mars Mechanical engineering Nonlinearity Pressure distribution Propeller blades Reynolds number Simulation Wind tunnels
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