the chord line造句

• Often, the chord line of the coefficient of lift by definition.
• Initially, it was called the chord line.
• The Chord Line runs through the towns of Dankuni, Baruipara, Kamarkundu and Masagram.
• The angle of attack is the angle between the chord line of an airfoil and the oncoming air.
• Howrah to Bardhaman is reached by two corridors popularly known as the Main Line and the Chord Line.
• But between the leading and trailing edge the camber line can curve above or below the chord line.
• The camber value specified here gives the highest value above or below the chord line divided by the chord length.
• Decalage angle can also refer to the difference in angle of the chord line of the wing and the chord line of the horizontal stabilizer.
• Decalage angle can also refer to the difference in angle of the chord line of the wing and the chord line of the horizontal stabilizer.
• When the chord line is horizontal, the trailing edge has a downward direction and since the air follows the trailing edge it is deflected downward.
• Pressure differences result from is the chord line of the sail and the apparent wind velocity ( "'V A "').
• It runs along the chord line through the shortest route to Chennai via Nagercoil, Tirunelveli, Madurai, Virudhunagar, Trichy, Villupuram and Chengalpattu.
• The mean camber line is an imaginary line which lies halfway between the upper surface and lower surface of the airfoil and intersects the chord line at the leading and trailing edges.
• Construction of the chord line might not have been justified with the current level of traffic ( now that Eurostar trains no longer use the route through Shortlands to and from Waterloo ).
• Earlier, nine rake EMU coaches were used in local trains but twelve coach EMU trains have been introduced in the chord line in 2011, for which the platforms have been extended.
• In aerodynamics, angle of attack specifies the angle between the chord line of the wing of a fixed-wing aircraft and the vector representing the relative motion between the aircraft and the atmosphere.
• The H . P . 51 was powered by two 750 hp ( 560 kW ) Armstrong Siddeley Tiger IV 14-cylinder double-row radial engines mounted on the chord line and in broad-chord Townend cowlings.
• When symmetric aerofoils are moving parallel to the cambered aerofoils are moving parallel to the chord line, lift is generated . ( See diagram at right . ) For symmetric aerofoils, the chord line and the zero lift line are the same.
• When symmetric aerofoils are moving parallel to the cambered aerofoils are moving parallel to the chord line, lift is generated . ( See diagram at right . ) For symmetric aerofoils, the chord line and the zero lift line are the same.
• The " aerodynamic center " is defined to be the point on the chord line of the airfoil at which the " pitching moment coefficient " does not vary with angle of attack, or at least does not vary significantly over the operating range of angle of attack of the airfoil.