The fin
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
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
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
B. S. Campion has written: 'Estimation of the effects of distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers)'
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.
The longitudinal stability of an airplane is primarily determined by the location of the center of gravity (CG) in relation to the aerodynamic center of the wing. If the CG is in front of the aerodynamic center, the airplane tends to be stable. If the CG is too far behind the aerodynamic center, the airplane can become unstable. Pilots use the elevator control surface to adjust the pitch and maintain longitudinal stability.
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.
To impart a longitudinal spin to a projectile which gives gyroscopic stability to the projectile which greatly increases its accuracy.
Arabian sea
what is telebrix and the side effects.