The location of the CG with respect to the center of lift.
The longitudinal arm of an R22 helicopter is the distance from the center of gravity to the main rotor shaft. It is an important parameter for calculating balance and stability of the helicopter during flight.
Paper airplanes fly due to the principles of aerodynamics. The factors that contribute to their flight capabilities include the design of the airplane, the weight distribution, the shape of the wings, and the force of the throw. The design of the airplane affects its stability and lift, while the weight distribution and shape of the wings impact its ability to stay in the air. The force of the throw determines the initial speed and trajectory of the airplane.
Longitudinal feed refers to the movement of the cutting tool along the length of the workpiece during a machining operation. It determines the rate at which material is removed from the workpiece and influences the surface finish and efficiency of the machining process.
The lateral longitudinal arch of the foot helps distribute body weight along the outer edge of the foot during walking and running. It provides stability and support to the foot by absorbing shock and adapting to uneven surfaces.
The three movements of an airplane are pitch (upward and downward movement along the lateral axis), roll (side-to-side movement along the longitudinal axis), and yaw (rotation around the vertical axis). These movements are controlled by the elevator, ailerons, and rudder, respectively.
The shape of the fuselage and fin improve longitudinal stability.
F. G. Irving has written: 'An introduction to the longitudinal static stability of low-speed aircraft' -- subject(s): Longitudinal Stability of airplanes, Stability of airplanes, Longitudinal
S. M. Cooley has written: 'Determination of airplane longitudinal stability derivatives from transient responses' -- subject(s): Aeronautics
The fin
William T. Suit has written: 'Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data' -- subject(s): Lateral Stability of airplanes, Longitudinal Stability of airplanes, Stability of airplanes, Lateral, Stability of airplanes, Longitudinal
It's longitudinal axis
C. Van de Kreeke has written: 'The interference of the model support mast with measurements of the longitudinal and lateral aerodynamic coefficients' -- subject(s): Lateral Stability of airplanes, Longitudinal Stability of airplanes, Stability of airplanes, Lateral, Stability of airplanes, Longitudinal
James M Luckring has written: 'Theroetical and experimental analysis of longitudinal and lateral aerodynamic characteristics of skewed wings at subsonic speeds to high angles of attack' -- subject(s): Aerodynamics, Airplanes, Lateral Stability of airplanes, Longitudinal Stability of airplanes, Stability of airplanes, Lateral, Stability of airplanes, Longitudinal, Wings
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Longitudinal directional stability refers to the ability of an aircraft to maintain its heading when disturbed by external forces, such as turbulence or control inputs. It is achieved through proper design of the aircraft's aerodynamic characteristics, including the location of the center of gravity relative to the center of lift. Strong longitudinal directional stability helps pilots maintain control of the aircraft in various flight conditions.
Because you ride in it, and they are expensive.
The longitudinal arm of an R22 helicopter is the distance from the center of gravity to the main rotor shaft. It is an important parameter for calculating balance and stability of the helicopter during flight.