Timeline for How can the zero-lift drag coefficient (parasitic drag) be calculated?
Current License: CC BY-SA 3.0
3 events
| when toggle format | what | by | license | comment | |
|---|---|---|---|---|---|
| Jan 19, 2018 at 13:58 | comment | added | Koyovis | The minimum flight speed is at maximum $C_L$, where the wing stalls. | |
| Jan 19, 2018 at 5:22 | comment | added | Josh Pilipovsky | so how would I be able to solve for the minimum flight speed? | |
| Jan 19, 2018 at 4:36 | history | answered | Koyovis | CC BY-SA 3.0 |