## In reference to a nonlinear theory of aerodynamic stability |

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3mall AERODYNAMIC STABILITY approximations are determined approximations will grow boundaries of stability boundary conditions boundary layer change of perturbations character of change complex functions Consequently corresponding equation development of perturbations dx dy dy dx form function of perturbed GOVERNMENT RESEARCH REPORT In-this laminar flows linear theory linearized problem liquid modified system mombers motion will satisfy nonlinear theory nonuniform differential obtain the following Office of Technical ordinary differential equations parallel walls parameter partial solution periodic functions perturbed motion quadratures recurrence system regions of unstable Reports and translations Reynolds number satisfy equation small perturbations speed component stability and character stability of laminar stream function subsequent approximations successive approximations system of complex system of differential system of equations system of ordinary Technical Services THEORY OF AERODYNAMIC theory of stability theory stable Tho solution U. S. Department U. S. GOVERNMENT unstable flows unstable region USSR V. V. Struminskiy