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summary
Increments in aerofoil lift coefficient at zero angle of attack and in maximum lift coefficient due to deployment of a single-slotted trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
Details
Publisher
ESDU
File size
343.88 KB
Pages
27
Format
PDF
Publication date
1995
ISBN-13
978-0-856-79917-4
ISBN-13 plain
9780856799174
ISBN-10
1015202530
