Sentence examples for maximum lift coefficients from inspiring English sources

Standard airfoils historically used for wind and hydrokinetic turbines have the maximum lift coefficients of about 1.3 at the stall angle of attack, which is about 12°.

Standard airfoils historically used for wind and hydrokinetic turbines had maximum lift coefficients of around 1.3 at stall angles of attack, which is about 12°.

At the Reynolds numbers of 75,000, 128,000 and 205,000, maximum lift coefficients of 1.72, 1.81 and 1.86 respectively were obtained at the stall angle of 14°.

The work by Song et al. [59] indicates that compliant, membrane wings achieve greater maximum lift coefficients than rigid wings, but data have yet to be collected demonstrating that this holds in vivo for bats and birds.

Membrane wings are able to provide higher maximum lift coefficients than avian wings, and the membranous wings of bats are expected to have a steeper lift slope than the stiffer, less compliant wings of birds [59].

High camber increases the maximum lift coefficient.

until a maximum lift coefficient value at which point the wing flow stalls and lift reduces.

The testing verified the high lift/drag ratio and the high maximum lift coefficient for the WT180 airfoil.

Using leading edge slat delays the stall up to an angle of attack with a maximum lift coefficient.

In addition, it can also increase stall angle and maximum lift coefficient, and postpone the decrease in the gradient of the lift coefficient.

Comparatively, the aerodynamic performances of the new airfoil such as maximum lift coefficient, maximum lift-drag ratio, roughness insensitivity and so forth are better than the DU93-W-210 airfoil performances.