PARSEC airfoil polynomial coefficient solver

버전 1.1.0.0 (921 Bytes) 작성자: Sean Wu
Determines the airfoil polynomial coefficients for a given set of PARSEC geometric parameters.
3.0
(2)
다운로드 수: 569
업데이트 날짜: 2015/3/21

라이선스 보기

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

인용 양식

Sean Wu (2024). PARSEC airfoil polynomial coefficient solver (https://www.mathworks.com/matlabcentral/fileexchange/50138-parsec-airfoil-polynomial-coefficient-solver), MATLAB Central File Exchange. 검색됨 .

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개발 환경: R2014b
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버전 게시됨 릴리스 정보
1.1.0.0

Fixed missing parenthesis.
1.0.0.0