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  2. Dynamic stall on helicopter rotors - Wikipedia

    en.wikipedia.org/wiki/Dynamic_stall_on...

    The effect of dynamic stall limits the helicopter performance in several ways such as: The maximum forward flight velocity and thrust; High blade structural loads, which may result in excessive vibrations and blade structural damage; Control system loads, manoeuvre capability, and handling qualities; Helicopter dynamic performance.

  3. Category:Helicopter aerodynamics - Wikipedia

    en.wikipedia.org/wiki/Category:Helicopter...

    Pages in category "Helicopter aerodynamics" The following 23 pages are in this category, out of 23 total. ... Dynamic rollover; Dynamic stall on helicopter rotors; F.

  4. Helicopter flight controls - Wikipedia

    en.wikipedia.org/wiki/Helicopter_flight_controls

    Changes to the aircraft flight control system transmit mechanically to the rotor, producing aerodynamic effects on the rotor blades that make the helicopter move in a desired way. To tilt forward and back (pitch) or sideways (roll) requires that the controls alter the angle of attack of the main rotor blades cyclically during rotation, creating ...

  5. Helicopter dynamics - Wikipedia

    en.wikipedia.org/wiki/Helicopter_dynamics

    Its comprises helicopter aerodynamics, stability, control, structural dynamics, vibration, and aeroelastic and aeromechanical stability. [1] By studying the forces in helicopter flight, improved helicopter designs can be made, though due to the scale and speed of the dynamics, physical testing is non-trivial and expensive.

  6. Servo transparency - Wikipedia

    en.wikipedia.org/wiki/Servo_transparency

    A helicopter's main rotor hub. The vertical rods are at the end of the control chain that starts with the pilot controls. Helicopter flight controls are connected to the main and tail rotors, and include a cyclic stick, broadly to control forward-aft and left-right movements, a collective lever, broadly to control vertical movements, and anti-torque pedals, to control left and right yaw.

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  8. Stall (fluid dynamics) - Wikipedia

    en.wikipedia.org/wiki/Stall_(fluid_dynamics)

    As soon as it passes behind the trailing edge, however, the lift reduces dramatically, and the wing is in normal stall. [40] Dynamic stall is an effect most associated with helicopters and flapping wings, though also occurs in wind turbines, [41] and due to gusting airflow. During forward flight, some regions of a helicopter blade may incur ...

  9. Lighting on radio tower reportedly failed days before ...

    www.aol.com/fiery-helicopter-crash-topples...

    The aircraft departed Ellington Airport, which is about 17 miles south of the crash site. Rutt said the helicopter did not have a flight data recorder, which is not required.