Equations Flashcards

1
Q

Theoretical drag

A

Dynamic pressure x surface area

p/2 x v^2 x A

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2
Q

Theoretical lift

A

Dynamic pressure x surface area

p/2 x v^2 x A

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3
Q

Coefficient of lift

A

Measured lift / theoretical lift

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4
Q

Coefficient of drag

A

Measured drag / theoretical drag

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5
Q

Actual lift

A

Coefficient of lift x dynamic pressure x surface area

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6
Q

Actual drag

A

Coefficient of drag x dynamic pressure x surface area

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7
Q

Lift to drag ratio

Best glide ratio

A

Coefficient of lift / coefficient of drag

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8
Q

Thrust

A

D + Wsin(theta)

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9
Q

Lift

A

Wcos(theta)

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10
Q

Taper ratio

A

Tip chord / root chord

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11
Q

Power

A

Work / time

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12
Q

Acceleration

A

Change of speed / time taken

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13
Q

Aspect ratio

A

Wing span / average chord

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14
Q

Work

A

Force x distance

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15
Q

Bernoulli’s equation

A

Ptot = p + q

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16
Q

Wing area

A

Wing span x chord

17
Q

Speed

A

Distance / time

18
Q

Continuity equation

A

V1 x A1 = V2 x A2

19
Q

Mach number

A

Speed of the aircraft / speed of sound

20
Q

Speed of sound

A

a = 20 x square root T

21
Q

Pressure

A

Force / area

22
Q

Dynamic pressure

A

q = p/2 x v^2

23
Q

Force

A

Mass x acceleration

24
Q

Weight

A

Mass x gravitational acceleration

25
Q

Static pressure

A

Height x density x gravity