Performance - PowerPoint PPT Presentation

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Performance

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Remember that the rating is given in the brake horsepower output of the engine ... line 200 horsepower, the max. bph of the 200 horsepower engine. Not all ... – PowerPoint PPT presentation

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Title: Performance


1
Performance
  • Chapter 5
  • Lecture 10

2
Performance
  • What does performance mean?
  • What determines performance?
  • How fast will it climb, how quickly will it take
    off, land, or how far will it go.

3
Level of Performance
  • Airframe- in-flight performance depends on its
    drag characteristics.
  • Remember power is required to move something a
    specific distance per unit or time.
  • Power is a force times velocity
  • Power required at any given velocity is
    determined by multiplying the drag times velocity.

4
Power Curve
  • Plotting power drag a curve appears
  • This is the power required curve or the power
    curve
  • The power curve has nothing to do with the engine
  • The curve is simply the drag curve replotted in
    terms of drag
  • The term power required refers to the power
    required for level flight

5
Power Curve
  • Figure 5-1 p. 116
  • A power required curve for an airplane that
    indicates 200kts to fly, with a 160hp required
  • Remember that the rating is given in the brake
    horsepower output of the engine
  • The actual power available for thrust is
    determined by multiplying bhp x prop. efficiency

6
Figure 5-2 p. 117
  • The dotted line 200 horsepower, the max. bph of
    the 200 horsepower engine
  • Not all 200 horsepower overcame drag
  • The amount available is the thp, which is the bhp
    x prop efficiency
  • Prop efficiency is always less than one, so thp
    is always less than bhp

7
Efficiency
  • The efficiency is usually greatest in cruise
    decreases at lower speeds
  • Where the power available and the power required
    curves cross is the max level flight speed
  • Above that speed more power is required than is
    available

8
Figure 5-3 p. 118
  • Power curves showing max power available 75
    power
  • Sustaining the speed demands the required amount
    of power being delivered
  • Below that speed, increasingly more power is
    required to sustain level flight

9
Back side of the power curve
  • The curve changes direction and curls up on the
    low speed side of the speed range
  • This effect is due to increased induced drag in
    this region results in a reversed trend in
    power requirement with airspeed

10
Back side of the power curve
  • The back side of the power curve is usually very
    short due to minimum power speed is low
  • Many airplanes stall before reaching that slow
    speed

11
Climb Performance
  • The airplanes ability to climb is also
    determined by the power curve
  • Excess power is not used in level flight but is
    used in a climb
  • Excess power is also called power differential

12
Excess Power
  • The rate of climb at any speed is proportional to
    the amount of excess power
  • This is inversely proportional to weight
  • Figure 5-4 shows the power required curve the
    maximum power available curve with max power

13
Power Curves
  • Figure 5-4 p. 120
  • Figure 5-5 p. 121
  • Figure 5-6 p. 122
  • Figure 5-7 p. 122

14
Vx Vy
  • When do you use Vx Vy?
  • How are Vx Vy different?
  • Figure 5-8 p. 123

15
Terms
  • Calibrated Airspeed
  • Ceiling
  • No more excess power climbing ability is zero
  • Absolute Ceiling
  • Point where the curves touch is required for
    level flight
  • Service Ceiling
  • Rate of climb is only 100fpm

16
Power Curves
  • Figure 5-9 p. 124
  • Figure 5-10 p. 125
  • Figure 5-11 p. 125

17
Twin Engine Climb Performance
  • The power required is divided into two engines
  • Figure 5-13 p. 127
  • Twin that looses 50 looses up to 80 of
    performance and up to 90 of climb rate
  • This is due to loss of power, asymmetric thrust
    adds to drag climbing even harder

18
Descent Glide Performance
  • When there is a negative difference in power we
    get a negative climb rate
  • Sinking and the resulting vertical velocity is
    called rate of sink
  • Minimum rate of sink does not necessarily mean
    the best overall glide performance.
  • At a very low airspeed, the aircraft is moving
    slowly at minimum sink speed

19
Glide
  • The maximum glide distance would be obtained at
    the minimum ratio of rate of sink to forward
    speed
  • This speed corresponds to the point were power
    velocity touch
  • This is best glide speed
  • Figure 5-16 p. 130

20
Glide Ratio
  • The ratio of horizontal to vertical distance for
    a given amount of altitude
  • Glide distance altitude x L/D

21
Time Distance
  • Range
  • Endurance
  • Cruise Efficiency

22
Quiz on Lecture 10Chapter 5
  • Please take out a sheet of paper
  • Include todays date your name

23
Quiz on Lecture 10Chapter 5
  • Describe the back side of the power curve.
  • Compare and contrast absolute ceiling and service
    ceiling.
  • How do you determine glide distance?
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