Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3

Author: Gillis, Clarence L.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56E17
Link: https://digital.library.unt.edu/ark:/67531/metadc64367/

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