File:AngleOfClimb.jpg
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Captions
Captions
Best Angle of Climb for a jet and a propeller aircraft
Summary[edit]
| Description |
English: In a jet, maximum excess thrust normally
occurs at the airspeed where the thrust required is at a minimum (approximately L/DMAX). In a propeller airplane, maximum excess thrust normally occurs at an airspeed below L/DMAX and frequently just above stall speed |
| 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[edit]
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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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| This file has been identified as being free of known restrictions under copyright law, including all related and neighboring rights. | ||
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 17:05, 7 February 2021 | | 1,287 × 484 (85 KB) | Pi3.124 (talk | contribs) | 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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