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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