Theoretical Stability Derivatives of Thin Sweptback Wings Tapered to a Point With Sweptback or Sweptforward Trailing Edges for a Limited Range of Supersonic Speeds

Author: Malvestuto, Frank S., Jr.
Year: 1949
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1761
Link: https://digital.library.unt.edu/ark:/67531/metadc55001/

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