Calculated values of the aerodynamical loads on a tangent-ogive forebody compare well -with experimental data.
计算出的空气动力数据与实验结果吻合。
On the basis of the above, the mechanism is investigated by which the chine forebody can delay delta wing vortex burst.
在此基础上，对融合体前体延迟翼涡破裂的机理进行了深入探讨。
The paper gives variations in the forebody drag, the normal force and the pressure center in accordance with the Mach Numbers and the geometric parameters.
给出了前阻、法向力及压心随马赫数或几何参数的变化曲线。
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