Basics Flashcards
Moment Coefficient equation
Cm = M / q.S.L
What is aerodynamics
The behaviour of air flow around an object and the effect it has on it
List things to think about when designing in 2D
- Assumes infinite wing span
- Inaccurate for finite wings
- Approximation is invalid at wing tips
- Approximation is okay for wings with large AR
- For swept wings, the section and the coefficients need to be transformed accordingly
Reynolds number =
Re = pVl / u
p - density
u - viscocity
l - reference length
Mach number =
M = V/a
a - speed of sound
If 2 geometries are similar, the air flows are said to be …
Dynamically similar
List properties of Flow similarity
Cl1 = Cl2 Re1 = Re2 M1 = M2
- Streamline patterns are the same
Why is flow similarity useful
- Can do scaled tests in wind tunnel (cheaper)
To match Re of real sized objects, smaller models have to either …
- Have a higher density/pressure
- Lower temp/viscosity
- Higher velocity
List compressibility categories and there related Mach numbers
Incompressible - M<0.3
Subsonic - 0.3
For inviscid compressible flow what is Cl a function of
Cl = f(Mach)
For viscid incompressible flow what is Cl a function of
Cl = f(Reynolds)
What is the centre of pressure
The location where the resultant of a distributed load effectively acts on the body
Equation for Centre of Pressure
Xcp = - Mle / n
n - normal force
Mle - Moment
For small incidence:
Xcp = Mle / L
How does centre of pressure move with reducing lift
Xcp moves downstream as lift reduces (can be outside aerofoil)