Wind-Tunnel Investigation of Effect of Yawing on Lateral-Stability Characteristics 2: Rectangular N.A.C.A. 23012 Wing with a Circular Fuselage and a Fin

Author: Bamber, M. J.
Year: 1939
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-730
Link: https://digital.library.unt.edu/ark:/67531/metadc54993/

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