File:Effect of altitude on range at a constant weight.png
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Summary
| Description |
English: A flight conducted at high altitude has a greater true airspeed (TAS), and the power required is proportionately greater than when conducted at sea level. The drag of the aircraft at altitude is the same as the drag at sea level, but the higher TAS causes a proportionately greater power required. |
| Date | |
| Source | Pilot's Handbook of Aeronautical Knowledge, page 11-11 |
| Author | Federal Aviation Administration |
Licensing
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This image or file is a work of a Federal Aviation Administration employee, taken or made as part of that person's official duties. As a work of the U.S. federal government, the image is in the public domain in the United States.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 22:26, 2 July 2023 | | 2,232 × 1,798 (534 KB) | 痛 | Uploaded a work by {{label|Q335357}} from Pilot's Handbook of Aeronautical Knowledge, page 11-11 with UploadWizard |
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