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Wind-Tunnel Investigation at High Subsonic Speeds of Spoilers of Large Projection on an NACA 65A006 Wing With Quarter-Chord Line Swept Back 32.6 Degrees
Author:
Vogler, Raymond D.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51L10
Link:
https://digital.library.unt.edu/ark:/67531/metadc59876/
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