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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