PARSEC airfoil polynomial coefficient solver
Determines the airfoil polynomial coefficients for a given set of PARSEC geometric parameters.
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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
Cita come
Sean Wu (2026). PARSEC airfoil polynomial coefficient solver (https://it.mathworks.com/matlabcentral/fileexchange/50138-parsec-airfoil-polynomial-coefficient-solver), MATLAB Central File Exchange. Recuperato .
Riconoscimenti
Ispirato: Airfoil optimization using Xfoil and PARSEC geometric parameterization, CB2: Airfoil Optimization with GUI
Informazioni generali
- Versione 1.1.0.0 (921 Byte)
Compatibilità della release di MATLAB
- Compatibile con qualsiasi release
Compatibilità della piattaforma
- Windows
- macOS
- Linux
