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Transonic free-flight investigation of the longitudinal aerodynamic characteristics of a 1/10-scale steel-wing of the Northrop MX-775A missile with leading-edge extensions, inboard trailing-edge flaps, and a speed brake on the vertical tail
Author:
Arbic, Richard G
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SL55B07
Link:
https://digital.library.unt.edu/ark:/67531/metadc61180/
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