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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