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summary
Wing lift coefficient increment at zero angle of attack due to deployment of double-slotted or triple-slotted flaps at low speeds.
Details
Publisher
ESDU
File size
393.39 KB
Pages
26
Format
PDF
Publication date
1995
ISBN-13
978-4-050-55105-7
ISBN-13 plain
9784050551057
ISBN-10
4050551050