NASA NACA-RM-L56D05-1956
Static lateral stability and control characteristics of a model of a 45 degrees swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01

Standard No.

NASA NACA-RM-L56D05-1956

Release Date

1956

Published By

National Aeronautics and Space Administration (NASA)