Performance Flashcards

1
Q

Thrust from a propeller is greatest when the aeroplane is?

A

stationary

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2
Q

shaft power/brake power =

A

indicated horsepower - frictional losses

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3
Q

thrust horsepower is?

A

brake horsepower accounted for propeller inefficiency

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4
Q

power required is directly related to the

A

total drag

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5
Q

For a prop aeroplane, best range is achieved at what speed?

A

The speed for minimum drag, or, the best lift/drag ratio speed

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6
Q

The speed for best endurance is the speed that requires?

A

the minimum amount of power, or, Vmp.

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7
Q

The speed for best rate of climb can be found at the speed for

A

the best lift/drag ratio

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8
Q

Relevant to the power curves, the best angle of climb speed is found?

A

where the distance between thrust available and thrust required is greatest

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9
Q

Relevant to the power curves, the best rate of climb speed is found?

A

where the distance between power available and power required is greatest

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10
Q

The trig formula for angle of climb

A

sin = T - D / W

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11
Q

Regarding climb performance:

any increase in weight will result in a -

A

flatter flight path with a reduced rate of climb at a higher speed.

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12
Q

The trig formula for the gliding angle is

A

Tan = D / L

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13
Q

The best glide speed will always be found at the speed for -

A

maximum lift/drag ratio

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14
Q

Does an increase in weight affect the gliding angle

A

No, since it depends on the lift/drag ratio.

Note: The lift/drag ratio is independent of weight. An increase in weight needs a corresponding increase in total lift and, consequently, a greater lift and drag will result. The proportions remain exactly the same and the L/D ratio and glide angle thus remain unaltered.

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15
Q

Does an increase in weight affect the gliding time?

A

Yes

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16
Q

the centre seeking force of a spinning object is called?

A

centripetal force

17
Q

the opposite and equal force to centripetal force is called?

A

the centrifugal force

18
Q

For aerodynamics, centripetal force is called?

A

the horizontal component of lift

19
Q

Centripetal force is directly ? to the ? of the body, the ? of its ? and ? proportional to the ? of the turn.

A

Centripetal force is directly proportional to the mass of the body, the square of its speed and inversely proportional to the radius of the turn.

20
Q

Steep turns are considered to be in excess of

A

45 degrees

21
Q

Centripetal force in pounds =

A

W V^2 / g r

22
Q

How to calculate the stalling speed in a turn?

A

New stalling speed = Old stalling speed x square root of load factor

23
Q

How to calculate the load factor in a turn with a bank angle of 30?

A

load factor = n(1) / cos 30

24
Q

during a glide, the distance flown compared to increased weight, remains?

A

Unchanged

25
Q

A heavier aircraft will have a higher(vmd speed)?

A

maximum lift/drag ratio airspeed

26
Q

In a glide, added weight will reduce?

A

The glide endurance

27
Q

The ROC speed with altitude will -

A

increase