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summary
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: single, upper and lower surfaces geometry and camber line variations, initial aerofoil: NACA 0012 and RAE 2822, CFD: BVGK.
Details
Publisher
ESDU
File size
1.36 MB
Pages
28
Format
PDF
Publication date
2001
ISBN-13
978-2-074-90515-3
ISBN-13 plain
9782074905153
ISBN-10
2074905151
