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Summary
DescriptionMaximum Endurance and Range.jpg
English: The maximum endurance condition would be obtained at the
point of minimum power required since this would require the
lowest fuel flow to keep the airplane in steady, level flight.
Maximum range condition would occur where the ratio of
speed to power required is greatest. The maximum range condition is obtained at maximum lift/
drag ratio (L/DMAX)
Date
Source
Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/
Author
U.S. Dept. of Transportation, FAA
Licensing
Public domainPublic domainfalsefalse
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This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights.
https://creativecommons.org/publicdomain/mark/1.0/PDMCreative Commons Public Domain Mark 1.0falsefalse
Captions
Maximum Endurance and Range versus airspeed
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17:05, 7 February 2021
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Pi3.124
Uploaded a work by U.S. Dept. of Transportation, FAA from Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/ with UploadWizard
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