How is the lift formula in aerodynamics derived?

AI Thread Summary
The lift formula in aerodynamics, expressed as F = Lift coefficient x area x air density x velocity squared, is derived primarily from empirical data rather than a straightforward physical derivation. The lift coefficient is a crucial proportionality constant determined through experimental or numerical methods. More complex physical formulas exist for lift and drag, but they are not as commonly used due to their complexity. Buckingham's Pi Theorem is suggested as a relevant concept for understanding the derivation of this formula. Empirical methods remain the foundation for establishing the lift equation in aerodynamics.
ykobe23
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I'm currently doing the IB (equivalent to A levels) and we have to do a research on a subject and i took aerodynamics, specifically lift and can someone explain to me how the lift formula(F= Lift coeffecient x area x air density x velocity squared ) is found ?

Thank you very much
 
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It is found simply through empirical data. The lift coefficient is a proportionality constant that has to be found experimentally, numerically or, rarely, analytically. It isn't a robust physical formula. The more physical formulae for lift and drag are much more complicated.
 
ykobe23 said:
(F= Lift coeffecient x area x air density x velocity squared ) is found ?

Thank you very much

Search for Buckingham's Pi Theorem.
 
thanks very much !
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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