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  2. Advance ratio - Wikipedia

    en.wikipedia.org/wiki/Advance_ratio

    The advance ratio is critical for determining the efficiency of a propeller. At different advance ratios, the propeller may produce more or less thrust. Engineers use this ratio to optimize the design of the propeller and the engine, ensuring that the vehicle operates efficiently at its intended cruising speed, see propeller theory.

  3. Propeller (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Propeller_(aeronautics)

    The advance ratio of a propeller is similar to the angle of attack of a wing. A propeller's efficiency is determined by [30] ... Advance ratio; Axial fan design;

  4. Propeller theory - Wikipedia

    en.wikipedia.org/wiki/Propeller_theory

    The essence of the actuator-disc theory is that if the slip is defined as the ratio of fluid velocity increase through the disc to vehicle velocity, the Froude efficiency is equal to 1/(slip + 1). [2] Thus a lightly loaded propeller with a large swept area can have a high Froude efficiency.

  5. Cyclorotor - Wikipedia

    en.wikipedia.org/wiki/Cyclorotor

    3.2 High advance ratio thrust and symmetric lift. 3.3 Unsteady aerodynamics. 3.4 Noise. ... A cyclorotor, cycloidal rotor, cycloidal propeller or cyclogiro, ...

  6. Propeller - Wikipedia

    en.wikipedia.org/wiki/Propeller

    A propeller (often called a screw if on a ship or an airscrew if on an aircraft) ... Advance ratioRatio of freestream speed to tip speed;

  7. Blade element theory - Wikipedia

    en.wikipedia.org/wiki/Blade_element_theory

    This is a two-bladed propeller 3 ft. in diameter, with a uniform geometrical pitch of 2.1 ft. (or a pitch-diameter ratio of 0.7). The blades have standard propeller sections based on the R.A.F-6 airfoil (Fig. 6), and the blade widths, thicknesses, and angles are as given in the first part of Table I.

  8. Slowed rotor - Wikipedia

    en.wikipedia.org/wiki/Slowed_rotor

    Rotorcraft Aspect ratio (mu) diagram Drag type curves as a function of airspeed (simulated) Cruise combinations for rotor power, propeller and wings. For rotorcraft, advance ratio (or Mu, symbol ) is defined as the aircraft forward speed V divided by its relative blade tip speed.

  9. Aircraft engine controls - Wikipedia

    en.wikipedia.org/wiki/Aircraft_engine_controls

    In adjustable-pitch propeller control system, the pilot has to adjust the propeller pitch angle and thus angle of attack of the propeller blades (typically with a lever) to achieve the desired propeller rotational speed. The increased pitch (blade angle of attack) increases the load on the engine and therefore slows it down, and vice versa.