Investigations on the Stability, Oscillation, and Stress Conditions of Airplanes with Tab Control: First Partial Report. Derivation of the Equations of Motion and their General Solutions

Author:	Filzek, B.
Year:	1949
Document Type:	N/A
Series:	NACA Technical Memorandums
Report Number:	NACA-TM-1197
Link:	https://digital.library.unt.edu/ark:/67531/metadc64673/