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Rocket-Model Investigation of the Rolling Effectiveness of a Fighter-Type Wing-Control Configuration at Mach Numbers From 0.6 to 1.5
Author:
Strass, H. Kurt
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51I28
Link:
https://digital.library.unt.edu/ark:/67531/metadc59062/
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