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summary
Examples of the application of constrained multivariate optimisation techniques to the design of aerofoil sections. Design point: single, geometry var: LE and TE flaps, initial aerofoil: combat aircraft section, CFD: BVGK (inviscid), Euler code.
Details
Publisher
ESDU
File size
545.72 KB
Pages
33
Format
PDF
Publication date
2000
ISBN-13
978-2-074-90515-3
ISBN-13 plain
9782074905153
ISBN-10
2074905151
