Investigation in the Ames Supersonic Free-Flight Wind Tunnel of the Static Longitudinal Stability of the Hermes A-3B Missile at a Mach Number of 5.0

Author: Canning, Thomas N.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SA52C10
Link: https://digital.library.unt.edu/ark:/67531/metadc65346/

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