Bleeding control for improving internal waverider inlet self-starting ability

Z Fengyuan, H Guoping, X Chen - … Journal of Turbo & Jet-Engines, 2019 - degruyter.com
Internal waverider inlets (IWIs) are novel three-dimensional (3D) high-performance inward
turning inlets. However, they possess poor self-starting capacity when applied in a fixed …

INTEGRATED DESIGN OF FOREBODY/INLET WITH DUAL-WAVERIDER IN THE STREAM DIRECTION BASED ON DISCRETE ISO-CONTRACTION RATIO

W Wannan, X Yabin, W Liyao, Y Lianjie… - Chinese Journal of …, 2023 - lxxb.cstam.org.cn
The integrated forebody/inlet design is an essential enabler for air vehicles targeting
hypersonic flight regimes. The crux of this integrated design lies in achieving the …

[HTML][HTML] ADVANCES IN DESIGN AND OPTIMIZATION OF WAVERIDER——FROM HYPERSONIC TO WIDE-SPEED RANGE

L Wen, G ShuaiQi, L Yang, W FaMin… - Chinese Journal of …, 2024 - pubs-en.cstam.org.cn
Hypersonic vehicle is one of the key development objects of the worldwide main power of
space technology. Nowadays, this type of vehicles is advancing towards the increased …

不同反压下椭圆形隔离段流场特征与气动性能

王卫星, 李博, 郭荣伟 - 航空动力学报, 2010 - jasp.com.cn
在反压条件下, 对椭圆形等直隔离段进行了全三维数值仿真研究. 结果表明: 在对称的几何条件和
边界条件以及均匀来流条件下, 当来流马赫数较小时, 流场与激波串结构基本对称; …

唇罩内型面对内转式进气道流动特性影响研究

朱婷, 王卫星, 张仁涛, 李宥晨 - 推进技术, 2019 - tjjs.ijournals.cn
内转式进气道流场参数分布不均, 为改善进气道的流场结构, 提高其气动性能,
采用数值仿真方法开展了唇罩内型面对内转式进气道流动特性影响的研究. 研究结果表明 …

DESIGN AND ANALYSIS OF A NOVEL HIGH SPEED SHAPE-TRANSITIONED WAVERIDER INTAKE

ME Noftz - 2022 - hammer.purdue.edu
Air intakes are a fundamental part of all high speed airbreathing propulsion concepts. The
main purpose of an intake is to capture and compress freestream air for the engine. At …

Analyzing the flow pattern of inward turning inlet combined with variable-geometry

Z Fengyuan, G Huang, H Huihui, C Xia - 52nd AIAA/SAE/ASEE Joint …, 2016 - arc.aiaa.org
I. Introduction he internal waverider inlet (IWI) is a novel type of three-dimensional (3D) high-
performance inward turning inlet [1, 2]. Recently, it is popularly researched by aviation, such …

[引用][C] 局部收缩比处处一致的变截面高超声速内转式进气道设计方法

肖雅彬, 岳连捷, 高占彪, 陈立红, 张新宇 - 2012

[PDF][PDF] New Inward-Turning Compressive Parent Flowfield for Streamline-Traced Intakes

O Musa, G Huang, B Jin, S Mölder, Z Yu - researchgate.net
Recently, there has been a resurgence in the interest given to high-speed air-breathing
vehicles because of their potential for extending the speed and range of some military and …

Application of Compound Compressible Flow to a Boundary Layer in a Hypersonic Three-Dimensional Inlet

G Bussey, M Lewis - 49th AIAA Aerospace Sciences Meeting including …, 2011 - arc.aiaa.org
An efficient inlet is a crucial component in the operation of a scramjet-powered hypersonic
vehicle. An effective inlet must provide efficient compression, enough mass flow, a high …