In order to validate various turbulence models involved,adopting finite volume methods to discrete Reynolds averaged Navier-Stokes equation in arbitrary coordinates,LU-SGS and MUSCL difference scheme to solving the discrete equations,two-element NLR-7301 airfoil and DLR-F6 wing-body configurati.

Two computed models and a numerical method based on nonlinear discrete vortex method are presented to simulate the vortex flow about wing-body combinations.

The research on aerodynamic characteristics of wrap-around fin and wing-body combination was carried out at super high speeds in this dissertation.

Aerodynamic configuration conceptual design for a wing-body vehicle;

Wing-body vehicles may have very high lift-to-drag ratio and maneuverability,and high L/D will benefit to increase the landing precision,enlarge the flight corridor,decrease the peak heat flux and the over load.

The finite volume technique used by Kroll to calculate Euler equations is developed in this paper to solve wing-body flow.

The study of evolution of the flow over the wing-body combination along the model axis at high incidences;

The computation of a wing-body combination with aileron;

A finite volume scheme is used to solve Euler equations in order to simulate transonic high-angle-of attack flow over a wing-body combination.