Insights Blog
-- Browse All Articles --
Physics Articles
Physics Tutorials
Physics Guides
Physics FAQ
Math Articles
Math Tutorials
Math Guides
Math FAQ
Education Articles
Education Guides
Bio/Chem Articles
Technology Guides
Computer Science Tutorials
Forums
General Engineering
Mechanical Engineering
Electrical Engineering
Aerospace Engineering
Nuclear Engineering
Materials Engineering
Trending
Featured Threads
Log in
Register
What's new
Search
Search
Search titles only
By:
General Engineering
Mechanical Engineering
Electrical Engineering
Aerospace Engineering
Nuclear Engineering
Materials Engineering
Menu
Log in
Register
Navigation
More options
Contact us
Close Menu
JavaScript is disabled. For a better experience, please enable JavaScript in your browser before proceeding.
You are using an out of date browser. It may not display this or other websites correctly.
You should upgrade or use an
alternative browser
.
Forums
Engineering
Mechanical Engineering
What is the Theoretical Solution for Lift at High Angles of Attack for Airfoils?
Reply to thread
Message
[QUOTE="OrangeDog, post: 5448891, member: 584341"] Im at work now and can't check. ToWS only covers up to stall for their studies so I doubt it would be in there. I checked von Mises book "Theory of Flight" (my favorite aeronautics book by the way) and it only used the small angle approximation. For the life of me I can't remember where I found the high AoA solution... [/QUOTE]
Insert quotes…
Post reply
Forums
Engineering
Mechanical Engineering
What is the Theoretical Solution for Lift at High Angles of Attack for Airfoils?
Back
Top