Closed-Form Expressions of Lift and Moment Coefficients for Generalized Camber Using Thin-Airfoil Theory

被引:2
作者
Joseph, Cibin [1 ]
Mohan, Ranjith [1 ]
机构
[1] Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 600036, Tamil Nadu, India
关键词
D O I
10.2514/1.J060859
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:4264 / 4270
页数:7
相关论文
共 18 条
[1]  
Abbott I.H., 1959, Theory of Wing Sections
[2]  
Anderson J., 2017, Fundamentals of Aerodynamics, V6th
[3]   The load bearing vortex surface for the treatment of planar problems in the hydrofoil theory. [J].
Birnbaum, W .
ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1923, 3 :290-297
[4]  
Borwein J.M., 2013, Not. Am. Math. Soc, V60, P50, DOI DOI 10.1090/NOTI936
[5]  
Dulikravich G. S, 1997, AERODYNAMIC SHAPE IN, DOI [10.1007/978-3-7091-2658-5_10, DOI 10.1007/978-3-7091-2658-5_10]
[6]  
Glauert H, 1924, 910 AER RES COMM R M
[7]   Low-speed natural-laminar-flow airfoils: Case study in inverse airfoil design [J].
Gopalarathnam, A ;
Selig, MS .
JOURNAL OF AIRCRAFT, 2001, 38 (01) :57-63
[8]  
Katz J, 2019, AIAA SCIT 2019 FOR, P1, DOI [10.2514/6.2019-0864, DOI 10.2514/6.2019-0864]
[9]   Universal parametric geometry representation method [J].
Kulfan, Brenda M. .
JOURNAL OF AIRCRAFT, 2008, 45 (01) :142-158
[10]   Section Curve Reconstruction and Mean-Camber Curve Extraction of a Point-Sampled Blade Surface [J].
Li, Wen-Long ;
Xie, He ;
Li, Qi-Dong ;
Zhou, Li-Ping ;
Yin, Zhou-Ping .
PLOS ONE, 2014, 9 (12)