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。
2
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。
3
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.