The 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 /
by John P. Campbell and John W. Paulson.

APA Citation

Campbell, J. P., Paulson, J. W., United States. National Advisory Committee for Aeronautics., Langley Aeronautical Laboratory. (1944). The 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. Langley Field, VA: Langley Memorial Aeronautical Laboratory.

MLA Citation

Campbell, John P, John W Paulson, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory. The 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. Langley Field, VA: Langley Memorial Aeronautical Laboratory, 1944.

Warning: These citations may not always be complete (especially for serials).