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aamira...@gmail.com

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Feb 10, 2024, 12:57:46 PM2/10/24
to noc24-ae0...@nptel.iitm.ac.in
Hi,

I have a question about what is happening in this video at 00:26:21 -

http://www.youtube.com/watch?v=miBc_RfElMI#t=1581s.

In the last numerical ,why did we take the condition of 0.866(L\D)max??.

Thanks!



Reference Key - Key('StudentQuestionEntity', 5407413147009024, namespace='ns_noc24_ae02')

NOC24 AE02

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Feb 17, 2024, 1:05:38 PM2/17/24
to Discussion forum for Aircraft Design, aamira...@gmail.com
Dear Learner

The value of approximately 0.866 represents a condition at which the aircraft's aerodynamic performance, particularly its lift-to-drag ratio, is optimized. This means that for a given design, adjusting the dimensions to achieve L/D≈0.866 can result in improved overall performance, including reduced fuel consumption for a given mission profile.

Hope this clarifies your doubt.

Thanks
Prashant (TA)

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