File:Effect of altitude on range at a constant weight.png
Size of this preview: 744 × 599 pixels. Other resolutions: 298 × 240 pixels | 596 × 480 pixels | 953 × 768 pixels | 1,271 × 1,024 pixels | 2,232 × 1,798 pixels.
Original file (2,232 × 1,798 pixels, file size: 534 KB, MIME type: image/png)
 | This is a file from the Wikimedia Commons. Information from its description page there is shown below. Commons is a freely licensed media file repository. You can help. |
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
|
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.
|
 |
File history
Click on a date/time to view the file as it appeared at that time.
| 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 |
File usage
The following page uses this file:
