The viscous optimal shape design, via sp
β
Adriana Nastase
π
Article
π
1999
π
John Wiley and Sons
π
English
β 219 KB
The shape of a flying configuration is globally optimized if its camber, twist, thickness and the similarity parameters of its planform are determined in order to obtain a minimum drag at cruising Mach number. The optimum-optimorum (OO) theory of the author solves this problem by using a lower limit