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Basic Aircraft Design Part 6
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  • View Times: 23
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  • Update Date: 07 Aug 2023
  • Aircraft design
  • Coefficient of Lift
  • Zero lift angle of attack
  • numerical
Video Introduction

This video demonstrates a numerical zerolift angle of attack and finds CL with the given parameters of aircraft. 

This video is a continuation of Aircraft design part 5.

Full Transcript
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Cite
If you have any further questions, please contact Encyclopedia Editorial Office.
Loya, A. Basic Aircraft Design Part 6. Encyclopedia. Available online: https://encyclopedia.pub/video/video_detail/837 (accessed on 16 January 2026).
Loya A. Basic Aircraft Design Part 6. Encyclopedia. Available at: https://encyclopedia.pub/video/video_detail/837. Accessed January 16, 2026.
Loya, Adil. "Basic Aircraft Design Part 6" Encyclopedia, https://encyclopedia.pub/video/video_detail/837 (accessed January 16, 2026).
Loya, A. (2023, August 05). Basic Aircraft Design Part 6. In Encyclopedia. https://encyclopedia.pub/video/video_detail/837
Loya, Adil. "Basic Aircraft Design Part 6." Encyclopedia. Web. 05 August, 2023.
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