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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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