Formulas | Aerodynamics Flashcards
Load factor =
lift / weight
Wing loading =
Aircraft weight / wing area
Static pressure(p) =
N/m2
The unit for air density:
Air density(rho) =
kg / m3
KE =
1/2 rho x v2
Bernoulli’s theorum:
Static pressure + Dynamic pressure = constant`
Dynamic Pressure(q) =
1/2 rho v2
How to calculate turn radius -
Turn radius = TAS squared(m/s) / (g x tan bank angle)
knots to m/s -
0.5144
Finding load factor with bank angle -
Load Factor = 1 / cos bank angle
Approximately how long does it take to fly a complete circle during a horizontal steady co-ordinated turn with a bank angle of 45° and a TAS of 200 kts?
First find turn radius:
200 x 0.5144 = 100 m/s
Turn radius = TAS squared / 10 x tan bank angle
10 000 / 10 x tan45 = 1000m
Now find turn diameter:
1 000m x 2
= 2 000m
Now find circumference:
2 000 x 3.14 =
6280m
Now find time:
6280 / 100 m/s = 62.8s