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Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8
Author:
Schult, Eugene D
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54H17
Link:
https://digital.library.unt.edu/ark:/67531/metadc60629/
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