Free-flight investigation of longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, inline wings and tails

Author: Hall, James R
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51J17
Link: https://digital.library.unt.edu/ark:/67531/metadc59083/

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