This paper aims to provide some guidelines in the aerodynamic design and optimization of
future regional turboprop aircraft with about 90 passengers. Currently there are no …

采用自主开发的数值软件SPACER 对典型气动布局在 Ma= 6.0 (Re= 1× 107)
高超声速巡航时的气动力性能进行了数值评估. 评估的气动布局包括类乘波体(仿X-51A) …

The design and optimization of sensor array configurations is a significant challenge for
distributed SAR-GMTI radar systems because the system performance of distributed array …

This study presents a new method for aerodynamic optimization of a civil aircraft fuselage.
Typically, the fuselage is designed for minimum drag force at cruise conditions, which is …

In this work, a multi-objective optimization is applied for shape design of a civil aircraft
fuselage. Basically, a fuselage is not designed to generate the lift but, its drag force is so …

二次曲线由于其良好的几何特征, 在传统的飞机建模过程中得到较多的应用,
但是单一的控制参数使其外形变化受到限制, 而灵活的外形变化恰是NURBS 曲线的主要特点 …

Aerodynamic characteristics of traditional noses have been analyzed, and the deficiencies
of the aerodynamic shape of the noses are summarized. Streamline nose aerodynamic …

在1.2 m 量级亚跨超声速风洞采用DPIV, 测压, 油流显示三种实验技术对某型飞机机头模型气动
特性进行了实验研究, 得到了两个机头模型在巡航马赫数和快速巡航马赫数条件下的气动特性 …

Aerodynamic characteristics of traditional noses have been analyzed, and the deficiencies
of the aerodynamic shape of the noses are summarized. Streamline nose aerodynamic …

This paper aims to provide some gu the aerodynamic design and optim future regional
turboprop aircraft wit passengers. Currently there configurations on the market of this t …