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Longitudinal Stability and Drag Characteristics at Mach Numbers From 0.70 to 1.37 of Rocket-Propelled Models Having a Modified Triangular Wing
Author:
Chapman, Rowe, Jr.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52A31
Link:
https://digital.library.unt.edu/ark:/67531/metadc59113/
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