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Investigation at high subsonic speeds of the static lateral and directional stability and tail-loads characteristics of a model having a highly tapered swept wing of aspect ratio 3 and two horizontal-tail positions
Author:
Few, Albert G , Jr
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56E29
Link:
https://digital.library.unt.edu/ark:/67531/metadc62751/
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