Formulas | Aerodynamics Flashcards

1
Q

Load factor =

A

lift / weight

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2
Q

Wing loading =

A

Aircraft weight / wing area

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3
Q

Static pressure(p) =

A

N/m2

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4
Q

The unit for air density:

Air density(rho) =

A

kg / m3

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5
Q

KE =

A

1/2 rho x v2

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6
Q

Bernoulli’s theorum:

A

Static pressure + Dynamic pressure = constant`

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7
Q

Dynamic Pressure(q) =

A

1/2 rho v2

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8
Q

How to calculate turn radius -

A

Turn radius = TAS squared(m/s) / (g x tan bank angle)

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9
Q

knots to m/s -

A

0.5144

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10
Q

Finding load factor with bank angle -

A

Load Factor = 1 / cos bank angle

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11
Q

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?

A

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

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