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Flight measurements of the longitudinal stability, stalling, and lift characteristics of an airplane having a 35 degrees sweptback wing without slots and with 40-percent-span slots and a comparison with wind-tunnel data
Author:
Sjoberg, S. A.
Year:
1948
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1679
Link:
https://digital.library.unt.edu/ark:/67531/metadc54759/
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