Wind-Tunnel Measurements at Subsonic Speeds of the Static and Dynamic-Rotary Stability Derivatives of a Triangular-Wing Airplane Model Having a Triangular Vertical Tail

Author: Beam, Benjamin H.
Additional Authors: Reed, Verlin D.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A55A28
Link: https://digital.library.unt.edu/ark:/67531/metadc53200/

< New search