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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