Aerodynamic Flashcards

1
Q

Size of a fluid particle

A

1 μm

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2
Q

2D Body Definition

A

d/dxi = 0

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3
Q

Vorticity in 2D

A

ω = (δv/dx - δu/dy)k

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4
Q

Definition:

Streamline
Vortex Line
Smokeline/Streakline

A

Streamline tangent to velocity
Vortex Line tangent to vorticity
Smokeline/Streakline: line formed by particels that passed a certain point

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5
Q

Drag is..

A

A component of the aerodynamic force

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6
Q

parts of aerodynamic drag

A

Friction
Form drag
Wave drag (only for compressible flows)

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7
Q

Definition Reynolds number

A

L*U/ν

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8
Q

Main consequence on the flow due to the pressure of turbulence

A

diffusion is greatly increased

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9
Q

Mach number

A

M² =v²/a²

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10
Q

dimensionless coefficients c_l, c_d

A

= l/(0.5 ρU²c)

= d/(0.5 ρU²c)

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11
Q

Aspect Ratio R

A

AR = b²/S
if rectangular: AR = b/c
Delta Wing: R = 2 tan(Δ/2)

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12
Q

pressure and friction coefficient

A

= (p-p_infinity)/(0.5 ρU²c)
incrompressible, irrotational => 1

= τ/(0.5 ρU²c)

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13
Q

Airfoil nomenclature

A
LE leading edge
TE trailing edge 
Chord (tangent LE-TE)
Meanline 
Curvature t/c
Maximum thickness d/c
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14
Q

Lift coefficient in thin airfoil theory

A

C_l = 2π (α-α0)

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