Some Effects of Wing Height on the Vertical-Tail Pressure Distributions of a Complete Model in Sideslip at High Subsonic Speeds

Author: Few, Albert G., Jr.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57D22
Link: https://digital.library.unt.edu/ark:/67531/metadc63687/

< New search