Interactive ducational (ool for Classical Airfoil (Eeory Thomas J. Benson* NASA Lewis Research Center Cleveland, Ohio 44135 Oct
![Jousef Murad on Twitter: "⚡𝗡𝗔𝗖𝗔-𝟬𝟬𝟭𝟮 𝗔𝗶𝗿𝗳𝗼𝗶𝗹 𝗪𝗶𝘁𝗵 𝗗𝗲𝗽𝗹𝗼𝘆𝗶𝗻𝗴 𝗦𝗽𝗼𝗶𝗹𝗲𝗿⚡ Process of spoiler deviation is being modeling using method of viscous vortex domains (VVD). Re = 40 000. https://t.co/V4KJjjA9ER" / Twitter Jousef Murad on Twitter: "⚡𝗡𝗔𝗖𝗔-𝟬𝟬𝟭𝟮 𝗔𝗶𝗿𝗳𝗼𝗶𝗹 𝗪𝗶𝘁𝗵 𝗗𝗲𝗽𝗹𝗼𝘆𝗶𝗻𝗴 𝗦𝗽𝗼𝗶𝗹𝗲𝗿⚡ Process of spoiler deviation is being modeling using method of viscous vortex domains (VVD). Re = 40 000. https://t.co/V4KJjjA9ER" / Twitter](https://pbs.twimg.com/ext_tw_video_thumb/1614770253384372224/pu/img/TAvqFG0pwdwKZYcu.jpg:large)
Jousef Murad on Twitter: "⚡𝗡𝗔𝗖𝗔-𝟬𝟬𝟭𝟮 𝗔𝗶𝗿𝗳𝗼𝗶𝗹 𝗪𝗶𝘁𝗵 𝗗𝗲𝗽𝗹𝗼𝘆𝗶𝗻𝗴 𝗦𝗽𝗼𝗶𝗹𝗲𝗿⚡ Process of spoiler deviation is being modeling using method of viscous vortex domains (VVD). Re = 40 000. https://t.co/V4KJjjA9ER" / Twitter
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