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summary
Aerofoil and wing pitching moment coefficient increment at zero angle of attack due to deployment of leading-edge and trailing-edge high-lift devices in combination at low speeds.
Details
Publisher
ESDU
File size
449.24 KB
Pages
37
Format
PDF
Publication date
2003
ISBN-13
978-1-862-46170-3
ISBN-13 plain
9781862461703
ISBN-10
2074905151