The invention discloses a combined design method for an air-breathing hypersonic aircraft based on a conical flow field, which is characterized in that the design of the aircraft is divided into a forebody design, a wing design and a center body design on the basis of a reference conical flow field, and the block combined design of the air-breathing hypersonic aircraft is realized. According to the method, the efficient waverider characteristic of the aircraft can be met, combination of all parts of the hypersonic aircraft can be achieved, and a new optional design scheme can be provided for the aerodynamic layout of the air-breathing hypersonic aircraft in the future.
本发明公开了一种基于锥型流场的吸气式高超声速飞行器组合设计方法,以基准圆锥流场为基础,将飞行器的设计分为前体设计、机翼设计和中心体设计,实现吸气式高超声速飞行器分块组合设计。本发明不但可以满足飞行器的高效乘波特性,还可实现高超声速飞行器各部件组合,可以为未来吸气式高超声速飞行器气动布局提供一种新的可选设计方案。
Combined design method of air-breathing hypersonic aircraft based on conical flow field
一种基于锥型流场的吸气式高超声速飞行器组合设计方法
2022-06-24
Patent
Elektronische Ressource
Chinesisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Modular Hypersonic Inlets with Conical Flow
NTIS | 1968
|NTIS | 1990
|Hypersonic Air-Breathing Propulsion
AIAA | 2011
|