Performance Characteristics 1 Flashcards

1
Q

What is best angle of climb?

A

The most altitude gained in the least amount of horizontal space (L/D Max airspeed)

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2
Q

What does best angle of climb depend on ?

A

Excess thrust

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3
Q

What is best rate of climb?

A

The most altitude gained in the shortest amount of time

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4
Q

What does best rate of climb depend on?

A

Excess power

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5
Q

Where does best angle of climb occur at on a lift drag curve?

A

L/D Max

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6
Q

How does weight affect climb angle and rate performance?

A

It decreases both

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7
Q

How does pressure altitude affect climb angle and rate performance?

A

It decreases both of them

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8
Q

How does wind affect climb rate or angle?

A

Wind does not affect climb rate or angle, only the climb gradient

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9
Q

What airspeed must you fly at to achieve max glide ratio?

A

L/D Max airspeed (230 KCAS + 1 knots for every 100 lbs of fuel remaining)

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10
Q

How does weight affect max glide distance?

A

Weight does NOT affect glide distance. It causes a higher descent ate/airspeed. You will glide the same distance as a lighter aircraft, but it will take you less time to glide said distance.

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11
Q

How does configuration affect max glide distance?

A

Decreases glide distance and glide airspeed

Remember configuration changes decrease L/D Max

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12
Q

How does a headwind or tailwind affect glide?

A

Headwind decreases glide distance

Tailwind increases glide distance

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13
Q

What is Specific Fuel Consumption

A

SFC = FF/Thrust

The rate of fuel used per pound of thrust, it measures turbojet engine efficiency

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14
Q

What factors affect SFC?

A

Factors such as RPM, temperature, and altitude affect the performance and fuel efficiency of the engine

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15
Q

How does an increase in RPM affect SFC?

A

It decreases SFC

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16
Q

How does an increase in Altitude affect SFC?

A

Decreases SFC due to a temperature decrease

17
Q

How does an decrease in temperature effect SFC?

A

It decreases SFC

18
Q

When is a turbojet engine most efficient generally?

A

At high altitudes where the temperature is lower and high power settings

19
Q

Where does max range occur on this graph?

A

Max Range occurs at a point on a line from the origin tangent to the T_R Curve.

20
Q

How does an increase in weight affect max range?

A

Range increases if the extra weight is due to fuel, but decreases if the extra weight is payload other than fuel

21
Q

How does an increase in altitude affect max range?

A

Maximum range performance increases with altitude

22
Q

How does configuration affect max range?

A

Lowering the landing gear or speed brake increases the thrust required, which
shifts the curve up, decreasing max range

23
Q

How does wind effect max range?

A

Winds do not affect endurance (time airborne), but they do affect distance traveled and can affect the conditions necessary to maximize range. As you would expect, a headwind reduces range by reducing ground speed (which would be less than TAS), while a tailwind increases range

24
Q

How does weight effect max endurance?

A

You should consider weight factors other than fuel when analyzing the effect of weight. Obviously, more fuel means
increased endurance. A heavier aircraft achieves maximum endurance at a higher airspeed than a lighter aircraft of the same type.

Max endurance decreases

25
How does configuration affect max endurance?
Lowering gear, speed brake, and/or flaps decreases endurance
26
How does altitude affect max endurance?
Endurance increases with altitude
27
What is endurance?
Endurance is the total time an aircraft can remain airborne in level flight under specified conditions.
28
Max glide speed in a T-38 with 2000 lbs gas?
Max glide speed = 230 KCAS + 1 knot for every 100 lbs of fuel. Therefore, T-38 with 2000 lbs gas is: 230 KCAS + 20 = 250 KCAS
29
What is, generally, the T38 climb schedule?
The tech order climb schedule, described in the Diversion Range Summary chart, is essentially 500 KCAS at sea level minus 30 KCAS per 5,000 feet.
30
What is max range AOA?
0.18
31
What is max endurance AOA?
0.3
32
What is max range?
The best ratio of velocity to fuel flow. This airspeed gives us the highest TAS to TR ratio