File:Maximum Endurance and Range.jpg
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Summary
| Description |
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 |
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This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 17:05, 7 February 2021 | | 1,292 × 473 (153 KB) | 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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