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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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