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Free-Flight Investigation of the Rolling Effectiveness of a Wing-Spoiler Arrangement at High Subsonic, Transonic, and Supersonic Speeds
Author:
Sandahl, Carl A.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8A07
Link:
https://digital.library.unt.edu/ark:/67531/metadc57557/
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