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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 plain trailing-edge flap, with or without a leading-edge high-lift device, at low speeds.
Details
Publisher
ESDU
File size
282.33 KB
Pages
22
Format
PDF
Publication date
1994
ISBN-13
978-0-856-79915-0
ISBN-13 plain
9780856799150
ISBN-10
4050607080
