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POWER GRAPHS Performance

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POWER GRAPHSPOWER GRAPHS

PerformancePerformance

POWER GRAPHSPOWER GRAPHS

TOTAL DRAG (thrust required)

• Minimum drag speed

• Influence of weight

• Influence of altitude

POWER REQUIRED

• Minimum power required speed

• Influence of weight

• Influence of altitude

POWER AVAILABLE

• Influence of altitude

• Minimum and maximum speeds

TOTAL DRAGTOTAL DRAG

D

Ve

INDUCED DRAG

PA

RA

SIT

E D

RA

GTOTA

L D

RA

G

VMD

(max L/D ratio)

MINIMUM DRAG SPEEDMINIMUM DRAG SPEED

D

Ve

LOW WEIGHT

PA

RA

SIT

E D

RA

G

VMD1

HIGH WEIGHT

VMD2

INFLUENCE OF WEIGHTINFLUENCE OF WEIGHT

D

Ve

W = 20k

W = 10k

W = 30k

VMD1 VMD2 VMD3

INFLUENCE OF ALTITUDEINFLUENCE OF ALTITUDE

D

Ve

ANY LEVEL

INFLUENCE OF ALTITUDEINFLUENCE OF ALTITUDE

D

VTAS

SE

A L

EV

EL

1000

0 ft

2000

0 ft

DMIN = cte

SUMMARYSUMMARY

Induced drag decreases with speed, whilst parasite drag increases.

Flying at the minimum drag speed, parasite drag equals induced drag.

The minimum drag speed corresponds to max. L/D ratio speed.

If weight is increased, the minimum drag speed will be higher.

In terms of EAS, the minimum drag speed does not change with altitude.

In terms of TAS, the minimum drag speed increases with altitude, but the minimum drag value remains constant.

POWER REQUIREDPOWER REQUIRED

Pr

Ve

MINIMUM POWER REQUIRED

MINIMUM DRAG

(MAX L/D RATIO)

POWER = DRAG x SPEED

INFLUENCE OF WEIGHTINFLUENCE OF WEIGHT

Pr

Ve

W = 20k

W = 10k

W = 30k

INFLUENCE OF ALTITUDEINFLUENCE OF ALTITUDE

Pr

Ve

SEA LEVEL

1000

0 ft

2000

0 ft

VMin PR

INFLUENCE OF ALTITUDEINFLUENCE OF ALTITUDE

Pr

VTAS

SEA LEVEL

10000 ft

20000 ft

SUMMARYSUMMARY

The minimum power speed is lower than the minimum drag speed.

More weight obviously increases the power required.

Although the minimum power required increases with altitude, the minimum power required speed (EAS) remains constant.

Both minimum power required speed and minimum drag speed increase with altitude in terms of TAS.

POWER AVAILABLEPOWER AVAILABLE

Pa

Ve

FULL THROTTLE

80 %

50 %

INFLUENCE OF ALTITUDEINFLUENCE OF ALTITUDE

Pa

Ve

SEA LEVEL

5000 ft

MIN & MAX SPEEDSMIN & MAX SPEEDS

Pa

VeVMIN VMAX

EXCESS OF POWER

MIN & MAX SPEEDSMIN & MAX SPEEDS

Pa

VeVMin PR

EXCESS OF POWER

LACK OF POWER

SPEED IS STABLE

SPEED IS UNSTABLE