XFLR5 PART4 TRANSITION PREDICTION | XFLR5 HANDS ON TUTORIAL SERIES
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- Опубликовано: 21 авг 2024
- XFLR5 Hands on Tutorial Series
PART4 Transition Prediction
XFLR5
www.xflr5.tech/...
S809 airfoil geometry:
airfoiltools.com
Experimental results:
Dan M. Somers, Design and Experimental Results for the S809 Airfoil.
#xflr5 #xflr5airfoil #turbulent
Dr. Saqib great
Sir! Can you continue this series of videos pls:)? There are not enough sources except you,sir!
Yes sure I will be doing soon some new tutorials. Thanks for the feedback and nice comment.
@@Simulation-Engineer Thank you so much sir! I have an project to make a UAV so i would love to listen your advices about making UAV too.
Hi sir,
Can you explain how I can choose ncrit according to Reynolds number
ex: Re = 24000000 => Which value should I choose for Ncrit
Thank you
Ncrit is critical number in e^N theory (the disturbance in linearized bl equations grows e^N times before passing to turbulence).
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Ncrit values:
sailplane 12-14
motorglider 11-13
clean wind tunnel 10-12
average wind tunnel 9