Use of an Aerodynamically Pulsed All-Movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-Powered Models in Free Flight and Some Initial Results From an Arrow-Wing-Body-Tail Configuration

Author: Gillespie, Warren, Jr.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52C10
Link: https://digital.library.unt.edu/ark:/67531/metadc59187/

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