LLT iterative method

XFLR5 is an analysis tool for airfoils, wings and planes

Brought to you by: techwinder

LLT iterative method

Forum: Open Discussion

Creator: Nobody/Anonymous

Created: 2008-03-21

Updated: 2012-09-26

Nobody/Anonymous - 2008-03-21

Would anyone by able to tell me which iterative method XFLR5 uses when calculating the LLT method for wings, this would be the method used to calculate gamma(y) the circulation at a spanwise point, cheers Will

If you would like to refer to this comment somewhere else in this project, copy and paste the following link:
- Nobody/Anonymous - 2008-03-22
  
  The LLT implementation follows exactly the method described in NACA-TN-1269 :
  
  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930082188_1993082188.pdf
  
  The iteration method is described in § 5.8 of the guidelines
  
  andre
  
  If you would like to refer to this comment somewhere else in this project, copy and paste the following link:

Log in to post a comment.