At the same time, the effects of the Strouhal number and maximal attack angle on the hydrodynamics performance of the flexible fin were analyzed.

The frequency of oscillating excitation has more effect on improving aerodynamic performance of airfoil at large attack angle th.

This paper presents a numerical simulation of separated flow over an airfoil at large attack angles with oscillating excitations to study separation flow control over an airfoil.

Based on the characteristics of the complicated aerodynamics for the large attack angle air-to-air missile,using feedback linearization approach for the design of the flight control system is proposed.

Analysis of the unsteady character of the flow field at high incidence;

Investigation of pneumatic characteristics for a ventral S-shaped inlet at high incidence and low speed;

The process of primary vortices forming,lifting and shedding alternately along central axis from opposite sides of a slender body placed at high incidence to an oncoming stream is investigated numerically,and laws on axial evolution of its sectional flow-pattern topological structure are advanced.

A measurement technique for derivatives of aircraft due to acceleration in heave and sideslip at high angle of attack;

An application of the continuous scan technique to the high angle of attack fighter model test;

Analysis of supersonic flutter of the wing with high angle of attack with aerodynamics heating;

Analysis of high speed Reynolds number effect tests at high angles of attack;

The research of effect of flow turbulence on the aerodynamic characteristics of a wing body combination at high angles of attack;

This paper describes a wind tunnel free-flight technique for measuring pitch-damping derivatives of a missile model at high angles of attack.