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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 trailing-edge split flap, with or without a leading-edge high-lift device, at low speeds.
Details
Publisher
ESDU
File size
263.85 KB
Pages
23
Format
PDF
Publication date
1994
ISBN-13
978-0-856-79916-7
ISBN-13 plain
9780856799167
ISBN-10
2074905151
