Hermann Behrbohm

• A semi-numerical method for the determination of the disturbance velocity potential and the pressure distribution of double-delta wings with subsonic leading edges in supersonic flow: I. Symmetrical flow conditions
• A semi-numerical method for the determination of the disturbance velocity potential and the pressure distribution of double-delta wings with subsonic leading edges in supersonic flow: II. Uniform pitch and roll conditions
• Basic low speed aerodynamics of the short-coupled canard configuration of small aspect ratio
• On a minimum time flight path with regard to stress and heat limitations
• Optimal trajectories in the horizontal plane
• Optimal trajectories in the vertical plane
• Semi-discretized treatment of the equation of conduction of heat in solids
• The flat triangular wing with subsonic leading edges in sideslip at supersonic speeds
• The flat triangular wing with subsonic leading edges in steady pitch and roll at supersonic velocities
• The lifting trapezoidal wing with small aspect ratio at supersonic speed
• The method of upwash-cancellation in linearized supersonic wing theory as applied to the double-delta wing with subsonic leading edges. II. Velocity potential and pressure distribution at symmetrical flow conditions
• The method of upwash-cancellation in linearized supersonic wing theory as applied to the double-delta wing with subsonic leading edges: I. total lift and pitching moment in symmetrical flow conditions