Effect of high-lift devices on the static-lateral-stability derivatives of a 45 degree sweptback wing of aspect ratio 4.0 and taper ratio 0.6 in combination with a body

Author: Lichtenstein, Jacob H
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2819
Link: https://digital.library.unt.edu/ark:/67531/metadc56584/

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