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Theoretical Calculations of the Lateral Stability Derivatives for Triangular Vertical Tails with Subsonic Leading Edges Traveling at Supersonic Speeds
Note presenting pressure-distribution expressions and stability derivatives derived by use of linear theory for zero-end-plate triangular vertical tails with subsonic leading edges performing rolling, yawing, and constant-lateral-acceleration motions. Corresponding results for the sideslip motion, most of which have been previously reported, are also included.
Date:
December 1954
Creator:
Bobbitt, Percy J.
System:
The UNT Digital Library