Sentence examples for high angles of attack from inspiring English sources

The unified design method is applied to a highly maneuverable aircraft operating at high angles of attack.

Compared with a delta wing aircraft, the double-delta wing configuration has better aerodynamic performance at high angles of attack.

Due to the stall influence the airfoil presents sustained periodic and limit cycle oscillations at high angles of attack.

At moderate and high angles of attack, from 10° to 20°, the slot configuration outperforms the baseline configuration.

At high angles of attack such issues as Reynolds and Mach number scaling are further complicated by the presence of complex, unsteady separated flow structures.

Strong asymmetrical vortices appear on the leeward of slender body at high angles of attack, which has very unfavorable effect on the stability and control of the aircraft.

The work presented here examines the feasibility of applying SVMs to high angle-of-attack unsteady aerodynamic modeling field.

In this research, we explore the feasibility of a roll-pitch-yaw integrated autopilot for a high angle-of-attack missile.

Further, the effect of asymmetric center-of-gravity shift, post ejection of the store, on some complex high angle-of-attack maneuvers such as cobra and Herbst is also investigated.

This paper examines the impact on the steady states of the coupled roll yaw motion when using a high-order roll-dependent yaw moment, shown to be realistic up to angles of attack near 30°, in an effort to provide tools to explore the dynamic free-flight behavior in the high angle-of-attack regime.

As an example of an effective flow control framework, it is demonstrated that aerodynamic lift of a high angle-of-attack wing under fluctuating free-stream conditions can be stabilized using the DBD actuator and an adaptive algorithm based on general input output models.