Range + Endurance Flashcards
How is max range in level flight achieved?
When the greatest distance is covered for the amount of fuel used
SAR
Specific air range = air distance flown / fuel used
SFC
Specific fuel consumption is fuel flow per unit of power produced
Fuel flow
Units of fuel used per hour
Max SAR =
Max SAR = airframe efficiency (or TAS / power) x engine efficiency (1 / SFC)
How is max range achieved from an airframe efficiency perspective
By flying at the min drag speed (on a PR curve this occurs where the line draw from the origin of the graph is tangential to the curve)
Wind effect on range
Range reduces in headwind and increases in tailwind, in strong headwinds the optimum speed for range is increased and in strong tailwinds the optimum speed is reduced
Engine considerations for flying range
Lowest SFC and the best range is achieved by:
- having no more than weak mixture MAP set
- min RPM
- engine is properly leaned
- supercharger in low gear
- a/c at full throttle height
- carb heat OFF + air filter OUT
Altitude and Weight effect on range
Altitude has no effect on the best IAS to fly but if weight is increased range is reduced and the best speed to fly is increased