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summary
Example of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Dual design point, upper and lower surface shape geometry, leading and trailing edge flap deflections, RAE 2822, Euler code and BVGK.
Details
Publisher
ESDU
File size
513.81 KB
Pages
21
Format
PDF
Publication date
2001
ISBN-13
978-2-074-90515-3
ISBN-13 plain
9782074905153
ISBN-10
2074905151
