Investigation of a Novel Configuration Concept for Airbreathing Hypersonic Vehicles
A novel forebody-inlet integration design concept is proposed in this paper. This design incorporates the advantages of waveriders and conventional 2dimensional inlets design. Based on the proposed design concept, a novel airbreathing hypersonic vehicle configuration was developed. The aerodynamic characteristics and control characteristics of this configuration were investigated. The investigation results indicate that the aerodynamic characteristics of this configuration, including lift-to-drag ratio, longitudinal stability, latitudinal stability and aero-surface control effectiveness, are very satisfactory.
Hypersonic configuration airframe-propulsion integration waverider
Chen Bingyan Zhou Weijiang Ji Chuqun Bai Peng
China Academic of Aerospace Aerodynamics, Beijing, P.R.China, 1000740 China Academic of Aerospace Aerodynamics, Beijing, P.R.China, 100074
国际会议
The 8th Sino-Russia High-speed Flow Conference(第八届中俄高超声速流体力学研讨会)
上海
英文
98-107
2011-11-21（万方平台首次上网日期，不代表论文的发表时间）