A review of the shock-dominated flow in a hypersonic inlet/isolator

H Huang, H Tan, F Li, X Tang, Y Qin, LB Xie… - Progress in Aerospace …, 2023 - Elsevier
A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

Recent advances and prospects in hypersonic inlet design and intelligent optimization

Y Ma, M Guo, Y Tian, J Le - Aerospace Science and Technology, 2024 - Elsevier
As the “respiratory tract” of the air breathing engine, the hypersonic inlet plays the role of
compressing, decelerating, and pressurizing flow. However, research on the traditional inlet …

Design and analysis of the air-breathing aircraft with the full-body wave-ride performance

T Zhang, X Yan, W Huang, X Che, Z Wang… - Aerospace Science and …, 2021 - Elsevier
Waverider is expected to break the lift-to-drag ratio constraint in the hypersonic flight
condition and it is commonly been studied as the forebody of the cruise vehicle. In this …

Performance analysis of the hypersonic vehicle with dorsal and ventral intake

S Luo, Y Sun, J Liu, J Song, W Cao - Aerospace Science and Technology, 2022 - Elsevier
The integrated design of the airframe and inlet is the favorite choice for the aerodynamic
configuration design of the air-breathing hypersonic vehicle. To better understand the …

Dynamic multi-objective optimization of scramjet inlet based on small-sample Kriging model

Y Ma, M Guo, Y Zhang, J Le, Y Tian, S Tong… - Physics of …, 2023 - pubs.aip.org
The generic inlet is depicted based on a smooth Bézier curve, and the results and insights
from high-dimensional dynamic multi-objective optimization of small-sample high Mach …

Aerodynamic analysis of an airframe-inlet integrated full-waverider vehicle designed by osculating cone theory

S Luo, J Tian, D Wang, C Zhang, H Yi - Acta Astronautica, 2024 - Elsevier
Recently proposed, the airframe/inlet integrated full-waverider vehicle design methodology
introduces an innovative approach to the design of air-breathing hypersonic vehicles. This …

Upgraded design methodology for airframe/engine integrated full-waverider vehicle considering thrust chamber design

Y Zhou, Z Xia, F Ding, W Huang - Acta Astronautica, 2023 - Elsevier
An upgraded airframe/engine integrated design approach for a full-waverider vehicle
considering thrust chamber design is proposed. Compared with the existing design …

Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp

L Chen, Y Zhang, H Xue, H Tan, Z Wang… - Aerospace Science and …, 2023 - Elsevier
When integrated with supersonic/hypersonic flight vehicles the ramp shock/boundary layer
interaction occurs in streamline-traced inward-turning inlets exhibit complex three …

Numerical investigation of real-gas effect of inward-turning inlet at Mach 12

C Dai, B Sun, C Zhou, C Zhuo, L Du, S Zhou - Aerospace Science and …, 2021 - Elsevier
To investigate the influence of the real-gas effect on the flow of the inward-turning inlet while
an air-breathing propulsion system flies at a high Mach number, gas models of thermally …

基于局部偏转吻切方法的多级压缩乘波体设计

郑晓刚, 朱呈祥, 尤延铖 - 力学学报, 2022 - lxxb.cstam.org.cn
乘波体因优异的气动特性, 被认为是突破现有“升阻比屏障” 的有效途径之一,
已成为高超声速飞行器气动设计的研究热点. 针对常规单级压缩乘波前体压缩量不足的问题 …