The Static and Dynamic-Rotary Stability Derivatives at Subsonic Speeds of an Airplane Model With an Unswept Wing and a High Horizontal Tail

Author: Buell, Donald A.
Additional Authors: Reed, Verlin D.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56I04
Link: https://digital.library.unt.edu/ark:/67531/metadc62922/

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