forebody

Calculated results of aerodynamic loads on a tangent-ogive forebody compare favorably with experimental data.

对一个切拱头体计算出的气动力特性与实验结果相符。

A new method of quickly hypersonic waverider forebody configurations was developed.

发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法.

Control of Forebody Flow Asymmetry in High-Angle Flows

大攻角前体非对称流动的控制技术

Smog visualization technique of asymmetric vortices on forebody at high wind speed

前体非对称涡高风速烟雾显示技术

The forebody design a key issue for hypersonic airbreathing vehicle.

前体设计是吸气式高超声速飞行器设计的关键之一.

A blended wing-body, variable camber wings, and forebody strakes provided extra lift and control.

翼身融合, 变曲率机翼, 还有前机身边条翼提供了额外的升力和控制性能.

When the separation distance is small, the region between two stages is filled with dead water flow, the bottom drag of forebody is negative, the typical afterbody effect phenomenon occurs.

级间距离较小时，级间区为死水区，前体阻力为负，出现典型的后体效应现象；

Influence of the Backward Jet of Afterbody on the Aerodynamic Characteristic of Forebody During Stage Separation

级间分离过程中后体反向喷流对前体气动特性的影响

Body configurations are composed of a blunt nosed forebody and 20 ° conical afterbody followed by a cylinder.

物体的形状由钝头前体和20°倒锥后接一个圆柱体构成。