Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45

Author: Wolowicz, Chester H.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-H56H03
Link: https://digital.library.unt.edu/ark:/67531/metadc64234/

< New search