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
Publisher: Langley Memorial Aeronautical Laboratory
Published: 1944
Place of publication: Langley Field, VA
Language: eng
Number of pages: 24
Subjects: Damping (Mechanics; Stability of airplanes, Longitudinal; Aerodynamics--Research.
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>