PARSEC airfoil polynomial coefficient solver

Version 1.1.0.0 (921 Bytes) by Sean Wu
Determines the airfoil polynomial coefficients for a given set of PARSEC geometric parameters.
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606 Downloads
Updated 21 Mar 2015

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This function determines a=[a1, a2, ...an] to solve the airfoil polynomial.
Zn=an(p)*X^(n-1/2), where n is the number of coordinates for the upper or
lower surface.
Input is a vector of PARSEC parameters p=[p1, p2, ...pn] where
p1=rle
p2=Xup
p3=Yup
p4=YXXup
p5=Xlow
p6=Ylow
p7=YXXlow
p8=yte
p9=delta yte (t.e. thickness)
p10=alpha te
p11=beta te
Information on the PARSEC airfoil parameterization is available at: http://www.as.dlr.de/hs/h-pdf/H141.pdf

Cite As

Sean Wu (2026). PARSEC airfoil polynomial coefficient solver (https://ch.mathworks.com/matlabcentral/fileexchange/50138-parsec-airfoil-polynomial-coefficient-solver), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2014b
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.1.0.0

Fixed missing parenthesis.
1.0.0.0