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Longitudinal Stability, Trim, and Drag Characteristics of a Rocket-Propelled Model of an Airplane Configuration Having a 45 Degree Sweptback Wing and an Unswept Horizontal Tail
Author:
Parks, James H.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52F05
Link:
https://digital.library.unt.edu/ark:/67531/metadc59229/
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