Sentence examples for angle of attack for from inspiring English sources

Typical examples investigated in aerodynamics are configurations at high angle of attack, for example an aircraft in landing configuration.

The sensitivity of the solution to the size of computational domain and the variation of the angle of attack for each type of BCs is also examined.

The predicted squeal sound level trend also compares well with that recorded at various crabbing velocities (proportional to angle of attack) for the test rig at different rolling speeds.

The average non-dimensional square root of the groove cross-section, l+, defined in terms of the drag coefficient at design angle of attack for the optimum riblet configuration in the fully coverage case was found to be l+≈10, which is very close to the optimum value found for planar surfaces.

The results from PIV and smoke flow visualization showed that the flow stayed fully attached to the airfoil surface from Re as low as 56,000 at an angle of attack of 8° and maintained a fully attached flow up to 14° angle of attack for Re as low as 75,000.

It is shown that the time history of the magnitude of the unsteady loading is almost completely unaltered by angle of attack for the step gust, but it's direction of action rotates forward by an angle equal to the angle of attack, extending an earlier result by Howe for a flat plate in a turbulent flow to airfoils of arbitrary thickness.

The angles of attack for highest lift-to-drag ratio for Hart Sports, Nordic Master 60 and Nordic Airglider javelins were found at 15°, 25° and 30° respectively.

Thus, Caudipteryx could have produced both lift and thrust during fast running by unfolding its wings at modest angles of depression and appropriate angles of attack for producing lift (Fig. 5d).

Specifically, Strouhal numbers and vibrational response were measured at a number of different angles of attack for both two- and three-dimensional models.

According to wind tunnel test results for angle of attack of 2° at Mach number M= 0.8, the porous configuration with 6.21% porosity results in a drag reduction of 0.0002 and lift drag ratio increase of 0.2, the small bump configuration results in a drag reduction of 0.0007 and lift drag ratio increase of 0.3.

This suggests for the aerodynamic features tested on the bat model that the leg-induced wing camber is a more important feature than the angle of attack of the tail membrane for controlling the level of lift produced.