An overview of research on wide-speed range waverider configuration

Z Zhao, W Huang, L Yan, Y Yang - Progress in Aerospace Sciences, 2020 - Elsevier
Hypersonic flight is becoming a common development goal of aeronautical and
astronautical technology, thus mandating the requirement that hypersonic vehicle have …

Hypersonic wavecatcher intakes and variable-geometry turbine based combined cycle engines

FY Zuo, S Mölder - Progress in Aerospace Sciences, 2019 - Elsevier
A summary is presented of research progress in the design and technology of hypersonic air
intakes and variable-geometry turbine based combined cycle (TBCC) intakes. Development …

An overview of research on waverider design methodology

F Ding, J Liu, C Shen, Z Liu, S Chen, X Fu - Acta Astronautica, 2017 - Elsevier
A waverider is any supersonic or hypersonic lifting body that is characterized by an attached,
or nearly attached, bow shock wave along its leading edge. As a waverider can possess a …

An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles

F Ding, J Liu, C Shen, W Huang, Z Liu, S Chen - Acta Astronautica, 2018 - Elsevier
A waverider is any supersonic or hypersonic lifting body that is characterized by an attached,
or nearly attached, bow shock wave along its leading edge. A waverider can possess high …

Integration of inward-turning inlet with airframe based on dual-waverider concept

Y Li, X Zheng, C Shi, Y You - Aerospace Science and Technology, 2020 - Elsevier
This paper proposes an inward-turning-inlet–forebody integration methodology based on
the dual-waverider concept. For the design concept and the designed flight conditions, both …

Novel inlet–airframe integration methodology for hypersonic waverider vehicles

F Ding, J Liu, C Shen, W Huang - Acta Astronautica, 2015 - Elsevier
With the aim of integrating a ramjet or scramjet with an airframe, a novel inlet–airframe
integration methodology for the hypersonic waverider vehicle is proposed. For this newly …

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 …

[HTML][HTML] 高超声速巡航飞行器乘波布局气动设计综述

王江峰, 王旭东, 李佳伟, 杨天鹏, 李龙飞, 程克明 - 空气动力学学报, 2018 - html.rhhz.net
吸气式高超声速乘波飞行器作为可以高效飞行于临近空间空域的运载器, 自概念提出以来一直
受到世界各国的高度关注, 并吸引着众多学者与机构对此开展研究. 本文主要从高超声速飞行器 …

Aerodynamic shape optimization of the vortex-shock integrated waverider over a wide speed range

F Qu, T Wang, C Liu, J Fu, J Bai - Aerospace Science and Technology, 2023 - Elsevier
The vortex-shock integrated waverider over a wide speed range could significantly improve
the aerodynamic performance of traditional waveriders by introducing the vortex effect at …

Assessment of new pressure-corrected design method for hypersonic internal waverider intake

O Musa, G Huang, Z Yu - Acta Astronautica, 2022 - Elsevier
The osculating axisymmetric flows concept is an extension of the concept of the osculating
cones for designing waveriders which is also utilized to design the three-dimensional …