Lateral Stability Investigation at Mach Numbers From 0.8 to 1.7 of Two Rocket-Boosted Models of an Airplane Configuration With a 45 Degree Swept Wing and a Low Horizontal Tail

Author: McFall, John C., Jr.
Additional Authors: Mitchell, Jesse L.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57G25
Link: https://digital.library.unt.edu/ark:/67531/metadc63690/

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