Aerodynamic Flashcards
Size of a fluid particle
1 μm
2D Body Definition
d/dxi = 0
Vorticity in 2D
ω = (δv/dx - δu/dy)k
Definition:
Streamline
Vortex Line
Smokeline/Streakline
Streamline tangent to velocity
Vortex Line tangent to vorticity
Smokeline/Streakline: line formed by particels that passed a certain point
Drag is..
A component of the aerodynamic force
parts of aerodynamic drag
Friction
Form drag
Wave drag (only for compressible flows)
Definition Reynolds number
L*U/ν
Main consequence on the flow due to the pressure of turbulence
diffusion is greatly increased
Mach number
M² =v²/a²
dimensionless coefficients c_l, c_d
= l/(0.5 ρU²c)
= d/(0.5 ρU²c)
Aspect Ratio R
AR = b²/S
if rectangular: AR = b/c
Delta Wing: R = 2 tan(Δ/2)
pressure and friction coefficient
= (p-p_infinity)/(0.5 ρU²c)
incrompressible, irrotational => 1
= τ/(0.5 ρU²c)
Airfoil nomenclature
LE leading edge TE trailing edge Chord (tangent LE-TE) Meanline Curvature t/c Maximum thickness d/c
Lift coefficient in thin airfoil theory
C_l = 2π (α-α0)