Title: Effects of static margin and rotational damping in pitch on the longitudinal stability characteristics of an airplane as determined by tests of a model in the NACA free-flight tunnel
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003614485&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003614485&ix=nu&I=0&V=D&pm=1</a>
Subjects: Damping (Mechanics, Stability of airplanes, Longitudinal, Aerodynamics--Research.