Post on 08-Jul-2015
Universidad San Francisco de Quito
Aerodinámica
Erik Proaño
Marco Teórico
Alerón Trasero (DRS desactivado)
Superficies
Streamlines
Campo Vectorial de Velocidades
Pressure Coutour
𝐿𝑖𝑓𝑡 = −6172,68202 [ 𝑁 𝑚]
𝐷𝑟𝑎𝑔 = 8358,291163 [ 𝑁 𝑚]𝑀𝑝𝑒𝑟𝑓𝑖𝑙 𝑠𝑢𝑝𝑒𝑟𝑖𝑜𝑟 = 1069,92881 [𝑁]
𝑀𝑝𝑒𝑟𝑓𝑖 𝑖𝑛𝑓𝑒𝑟𝑖𝑜𝑟 = 666,98191[𝑁]
Lift to Drag ratio
𝐿 𝐷 = 0,73851
Cálculos
Alerón Trasero (DRS activado)
Superficies
Streamlines
Campo Vectorial de Velocidades
Pressure Coutour
𝐿𝑖𝑓𝑡 = −3100,25735 [ 𝑁 𝑚]
𝐷𝑟𝑎𝑔 = 3686,293587 [ 𝑁 𝑚]𝑀𝑝𝑒𝑟𝑓𝑖𝑙 𝑠𝑢𝑝𝑒𝑟𝑖𝑜𝑟 = 409,81225 [𝑁]
𝑀𝑝𝑒𝑟𝑓𝑖 𝑖𝑛𝑓𝑒𝑟𝑖𝑜𝑟 = 311,90727[𝑁]
Lift to Drag ratio
𝐿 𝐷 = 0,841023
Cálculos
Abbott, I., & Von Doenhoff, A. (1959). Theory of Wing Sections. New York: Dover Publications.
Anderson, D. (2010).Fundamentals of Aerodynamics. Maryland .McGraw Hill.
White, F. (2008). Fluid Mechanics (6th ed.). Rhode Island: McGraw Hill.
Referencias