Your browser does not fully support modern features. Please upgrade for a smoother experience.
Basic Aircraft Design Part 5
- Subjects: Engineering, Aerospace
- |
- Contributor:
- Adil loya
- Aircraft
- Design
- Angle of Attack
- Coefficient of Lift
Video Introduction
This video demonstrates regarding the Angle of attack numerical, how to find AoA for unity lift coefficient and for per degree AoA.
This video is a continuation of Aircraft Design Part 4.
Full Transcript
${ textCharacter }/${ maxCharacter }
Submit
Cancel
Back
Comments
${ item }
|
${ item.createdUser.fullName }
${ item.createdAt }
${ item.vote }
${ item.reply }
Delete
${ reply.createdUser.fullName }
${ reply.createdAt }
${ reply.vote }
Delete
There is no reply to this comment~
${ item.replyTextCharacter }/${ item.replyMaxCharacter }
Submit
Cancel
More
No more~
There is no comment~
${ textCharacter }/${ maxCharacter }
Submit
Cancel
${ selectedItem.replyTextCharacter }/${ selectedItem.replyMaxCharacter }
Submit
Cancel
Confirm
Are you sure to Delete?
Yes
No
Cite
If you have any further questions, please contact Encyclopedia Editorial Office.
Loya, A. Basic Aircraft Design Part 5. Encyclopedia. Available online: https://encyclopedia.pub/video/835 (accessed on 13 May 2026).
Loya A. Basic Aircraft Design Part 5. Encyclopedia. Available at: https://encyclopedia.pub/video/835. Accessed May 13, 2026.
Loya, Adil. "Basic Aircraft Design Part 5" Encyclopedia, https://encyclopedia.pub/video/835 (accessed May 13, 2026).
Loya, A. (2023, August 04). Basic Aircraft Design Part 5. In Encyclopedia. https://encyclopedia.pub/video/835
Loya, Adil. "Basic Aircraft Design Part 5." Encyclopedia. Web. 04 August, 2023.
Copy Citation