Coefficients_of_Drag_and_Lift_vs_AOA.jpg (640 × 403 pixels, file size: 92 KB, MIME type: image/jpeg)
Summary
Coefficients of drag and lift versus angle of attack. Stall speed corresponds to the angle of attack at the maximum coefficient of lift U.S. Dept. of Transportation, FAA - Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/ Stall speed corresponds to the Angle of Attack at the Maximum Coefficient of Lift
Licensing
This file is in the public domain, because (no reason given!)
Please verify that the reason given above is valid! Note: if there is a specific licence tag for the reason supplied here, please use it. |
File history
Click on a date/time to view the file as it appeared at that time.
Date/Time | Thumbnail | Dimensions | User | Comment | |
---|---|---|---|---|---|
current | 10:33, 20 July 2023 | 640 × 403 (92 KB) | Isidore (talk | contribs) | Coefficients of drag and lift versus angle of attack. Stall speed corresponds to the angle of attack at the maximum coefficient of lift U.S. Dept. of Transportation, FAA - Pilot's Handbook of Aeronautical Knowledge, FFA-H-8083-25B, https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/phak/ Stall speed corresponds to the Angle of Attack at the Maximum Coefficient of Lift |
You cannot overwrite this file.
File usage
The following 2 pages use this file: