Takeoff, Climb, Cruise 323 Flashcards

1
Q

What is range?

A

How far an aircraft can fly by an airplane without having to refuel.

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2
Q

What is maximum range?

A

Maximum Range
o Minimum Drag
o Maximum L/D

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3
Q

For Prop Driven Airplanes Max Range means

A

♣ Prop Driven Airplanes: Max Range Means
o Max Fuel Load
o Minimum Fuel Consumption
o Max Prop Efficiency

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4
Q

Specific Range is the same on all aircraft?

T/F

A

False

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5
Q

What is endurance?

A

Total time an airplane stays in the air on a tank of fuel

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6
Q

ENDURANCE

For a prop driven plane you should

____ fuel consumption and use
_______ power required

Is endurance effected by wind?

A

♣ Propeller driven airplane
o Minimize fuel consumption
o Minimum power required (Vx Best Glide)

♣ Pull power and as you start to descend add power back in to stay level.
o Lower altitude is desirable

♣ HP required is lower

♣ KTAS is lower
o Lower Weight is desirable

♣ HP required is lower

♣ Ve(KTAS) is lower
o Endurance is not affected by wind, just trying to stay off the ground

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7
Q

What are variables for takeoff? (4)

A

Density
Wind
Runway Slope
Pilot Technique

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8
Q

How does density affect takeoff?

Temperature?
Pressure?
Moisture?

A

o Temperature
♣ High temperature means low density (longer takeoff roll)

o Pressure
♣ Low Pressure means low density

o Moisture
♣ High Humidity means Low Density

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9
Q

How does wind effect takeoff?

Where does the airplane start it’s takeoff roll?

What is the eqution for takeoff distance?
Does this work with all aircraft?

A

• Wind

o Airplane starts takeoff roll with Velocity equal to headwind component.

o Takeoff Distance = (Vlo-Vhw/Vlo)^2 (VERY IMPORTANT FOR YOUR LIFE FOREVER)

♣ Gives your actual takeoff distance
♣ Works with any aircraft because you calculate through POH and this gives wind value for real takeoff

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10
Q

How does Slope Effect takeoff distance?

Upslope?

Downslope?

What is the average ° slope on a runway? Does it really matter?

A

o Upslope
♣ Weight becomes the retarding force

o Downslope
♣ Weight becomes an accelerating force

o Most paved runways have less than 2 degree slope
THIS STILL HAS A SIGNIFICANT FORCE

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11
Q

How does pilot technique effect takeoff distance?

Too High of a speed?

Too Low of a speed?

Flaps?
First half of flap travel? (takeoff)
Second half of flap travel? (landing)

A

o Speed to high
♣ Increases distance (due to your rolling resistance)

o Speed too low
♣ Increases distance
• Induced drag (when you pull back that’s aerodynamic braking)

o Flaps

♣ First half of flap travel
• Big increase in lift (takeoff)
• Small increase in drag

♣ Second half of flap travel (For landing)
• Small increase in lift
• Big increase in drag

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12
Q

How can you minimize your ground roll? (3)

A

o Minimize weight
o Maximize Clmax
o Maximize surface area

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13
Q

How can you minimize takeoff distance? (1)

How is it done? (4)

A
•	Maximize acceleration
o	increase thrust
o	reduce drag
o	reduce weight
o	increase lift
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14
Q

What are the forces during take off? (3)

Define each one.

During Thrust ____ decreases as velocity increases.

Drag is initially ______ drag, but at lift off it is both ____ and _____ drag.

Friction is effected by what three things?

Rolling takeoffs take up ____ energy.

A

• Thrust (density altitude considerations etc.) (how much can I put out?)
o Decreases as velocity increases

• Drag
o Initially parasite drag
o Induced & parasite at liftoff

• Friction (rolling resistance of the aircraft)
o Forces acting on runway itself
♣ Surface
♣ Weight of the aircraft
♣ Lift (how much can you produce? The more you can make the less weight on wheels.)
♣ Rolling takeoffs take less energy

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15
Q

Takeoff basics:

Airplanes must accelerate from ______ to liftoff.

Liftoff speed is usually (equation)

Accleration = _____

A

• Airplanes must accelerate from 0 kts. To liftoff (disregarding winds)
• Liftoff speed is usually 1.2xVso
• Acceleration = A = Sum of all forces/Mass (don’t need to have for exam)
o Sum of forces over mass of object

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16
Q

What are complimentary angles?

A

Vx and Vy are complimentary, meaning If you climb at Vx or Vy your Vsi will rate the same regardless. Angle is what’s different. which changes the horizontal plane.

17
Q

Vx

What is it?

A

Vx Best Climb Angle

♣ Airspeed that provides greatest gain in altitude for the shortest horizontal distance.

18
Q

Vy

What is it?

A

Vy Best Rate of Climb Speed

♣ Airspeed that provides the greatest gain of altitude in the shortest time

19
Q

Angle of Climb

What is it. the effect of?
What does it do?
_____ but not. rate of climb.

A

♣ Effect of wind
o Reduces horizontal velocity ( travel shorter distance while climbing)
o Angle of climb changes but not rate of climb

20
Q

Cruise Climb

When is it used?
What is the usual cruise climb speed?
What are it’s benefits? (3)

A

♣ Used when traveling cross country

o Usually 10% below normal cruise speed
o High forward speed (wallet)
o Good rate of climb (regs)
o Excellent engine cooling (

21
Q

Normal High Speed Climb

This is seen a lot in what?

How do you calculate it?
Climb at en-route speed using ______.

At level off ______ is reduced.

A

Normal High-Speed Climb ( done a lot in the airlines)
♣ Calculate en-route speed (enroute speed = climb)
♣ Climb at en-route speed using climb power
♣ At level-off reduce to cruise power

22
Q

Cruise Flight:
What are the forces perpendicular to flight?

(5)

Descrbie

A

♣ Lift

♣ Weight

♣ Lift Weight coupling is the #1 force perpendicular to the flight path.

♣ Thrust Line – “Pendulum Effect” : any time thrust line does not equal the CG line on a horizontal plane or “water line”
o Nose up Or Down
o General rule of thumb – waterline is generally at the bottom of the windows.
o Engines above thrust line, cut in power makes it pitch up and vice versa.

♣ Drag
o Nose up or down
o Helps put the nose down or up tendency to even out the forces, but hurts performance.

♣ Weight
o Fuselage is just a de-stabilizing force

23
Q

What are the forces parallel to flight?

A

♣ Thrust

♣ Drag

24
Q

Any imbalance in forces will cause an

A

Acceleration or Deceleration.

25
Q

Straight and level flight, the sum of forces is __________

A

In equilibrium

26
Q

Three Factors of Maximum Level Cruise Speed

A

Altitude
Weight
Configuration

27
Q

Describe Maximum Level Cruise speed in regards to altitude.

A

Altitude provides better performance, less fuel use, and usualy stronger tailwinds.

28
Q

Describe weight in regards to Maximum Level Cruise

Forward CG provides you
Aft CG gives you
Worst peformance wth ___

Always fly with your CG right at the ____ limit but not past becuase you will be ____ and _____>

A

♣ Weight – how heavy you are (cost gas to carry gas) (CG & Taildown force) (tail down force only thing keeps you level)
o Forward CG – Lower TAS
o Aft CG – Higher TAS
o Worse performance with an Aft CG
♣ Always flight with CG right at the aft limit but not past)
• Flatter
• More slippery in the slipstream