![]() ![]() ![]() ![]() The L/D ratio is inversely proportional to the energy required for a given flightpath, so that doubling the L/D ratio will require only half of the energy for the same distance travelled. It depends principally on the lift and drag coefficients, angle of attack to the airflow and the wing aspect ratio. The L/D ratio is affected by both the form drag of the body and by the induced drag associated with creating a lifting force. It is measured empirically by testing in a wind tunnel or in free flight test. The L/D may be calculated using computational fluid dynamics or computer simulation. In almost all cases the graph forms a U-shape, due to the two main components of drag. These vary with speed, so the results are typically plotted on a 2-dimensional graph. The term is calculated for any particular airspeed by measuring the lift generated, then dividing by the drag at that speed. For a glider it determines the glide ratio, of distance travelled against loss of height. The L/D ratio for any given body will vary according to these flight conditions.įor an aerofoil wing or powered aircraft, the L/D is specified when in straight and level flight. It describes the aerodynamic efficiency under given flight conditions. In aerodynamics, the lift-to-drag ratio (or L/D ratio) is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic drag caused by moving through air. Lift and drag are the two components of the total aerodynamic force acting on an aerofoil or aircraft. ![]()
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