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aerodynamic Aeronautical Sciences aeroplane aircraft airfoil airplane altitude amplitude analysis angle of attack angular applied approximation aspect ratio assumed autopilot axis boundary conditions boundary layer calculated characteristics chord coefficient column component compressible flow compression computed considered constant curve cylinder damping damping ratio deflection derivatives determined downwash drag dynamic effect elastic engine equations of motion flight flow flutter force function given gust increase inertia inlet input integral Journal leading edge lift lift coefficient limit linear Mach Number maximum method missile modes nondimensional normal obtained operation oscillation panel paper parameters plan form plane plotted pressure problem range reference rudder servomechanism shear shock shown in Fig solution stability stability derivatives strain stress stress-strain curve structure subsonic supersonic surface tangent modulus tests theory tion triangular pulse turboprop variation vector velocity vertical vibration weight wing loading yaw damper zero