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Universidad San Francisco de Quito
AerodinΓ‘mica
Erik ProaΓ±o
Marco TeΓ³rico
AlerΓ³n Trasero (DRS desactivado)
Superficies
Streamlines
Campo Vectorial de Velocidades
Pressure Coutour
πΏπππ‘ = β6172,68202 [ π π]
π·πππ = 8358,291163 [ π π]πππππππ π π’ππππππ = 1069,92881 [π]
ππππππ ππππππππ = 666,98191[π]
Lift to Drag ratio
πΏ π· = 0,73851
CΓ‘lculos
AlerΓ³n Trasero (DRS activado)
Superficies
Streamlines
Campo Vectorial de Velocidades
Pressure Coutour
πΏπππ‘ = β3100,25735 [ π π]
π·πππ = 3686,293587 [ π π]πππππππ π π’ππππππ = 409,81225 [π]
ππππππ ππππππππ = 311,90727[π]
Lift to Drag ratio
πΏ π· = 0,841023
CΓ‘lculos
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
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