Flow quality in an M-Busemann wavecatcher intake

Feng Yuan Zuo; Sannu Mölder

doi:10.1016/j.ast.2022.107376

Flow quality in an M-Busemann wavecatcher intake

Feng Yuan Zuo
, Sannu Mölder

School of Aerospace Engineering

Toronto Metropolitan University

Research output: Contribution to journal › Article › peer-review

22 Scopus citations

Abstract

The detailed design steps and the idea of connecting M-flow and truncated Busemann flow are given in this paper. A new improved method is proposed to effectively reduce the size of the expansion zone in the original parent flowfield. The database of MBus parent flowfield at free-stream Mach 4 and Mach 6 is provided. Finally, a Mach-6 M-Busemann intake is designed to verify the performance of the improved parent flowfield. The CFD results show that the overall performance of M-Busemann intake has a good aerodynamic achievement, with a total pressure recovery reaching a very high value of 0.55. The influence of the calorically perfect model and thermally perfect model on the performance of the intake is not particularly obvious.

Original language	English
Article number	107376
Journal	Aerospace Science and Technology
Volume	121
DOIs	https://doi.org/10.1016/j.ast.2022.107376
State	Published - Feb 2022

Keywords

Busemann flow
Hypersonic
Streamline tracing
Wavecatcher intake

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10.1016/j.ast.2022.107376

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title = "Flow quality in an M-Busemann wavecatcher intake",

abstract = "The detailed design steps and the idea of connecting M-flow and truncated Busemann flow are given in this paper. A new improved method is proposed to effectively reduce the size of the expansion zone in the original parent flowfield. The database of MBus parent flowfield at free-stream Mach 4 and Mach 6 is provided. Finally, a Mach-6 M-Busemann intake is designed to verify the performance of the improved parent flowfield. The CFD results show that the overall performance of M-Busemann intake has a good aerodynamic achievement, with a total pressure recovery reaching a very high value of 0.55. The influence of the calorically perfect model and thermally perfect model on the performance of the intake is not particularly obvious.",

keywords = "Busemann flow, Hypersonic, Streamline tracing, Wavecatcher intake",

author = "Zuo, \{Feng Yuan\} and Sannu M{\"o}lder",

note = "Publisher Copyright: {\textcopyright} 2022 Elsevier Masson SAS",

year = "2022",

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doi = "10.1016/j.ast.2022.107376",

language = "英语",

volume = "121",

journal = "Aerospace Science and Technology",

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T1 - Flow quality in an M-Busemann wavecatcher intake

AU - Zuo, Feng Yuan

AU - Mölder, Sannu

PY - 2022/2

Y1 - 2022/2

N2 - The detailed design steps and the idea of connecting M-flow and truncated Busemann flow are given in this paper. A new improved method is proposed to effectively reduce the size of the expansion zone in the original parent flowfield. The database of MBus parent flowfield at free-stream Mach 4 and Mach 6 is provided. Finally, a Mach-6 M-Busemann intake is designed to verify the performance of the improved parent flowfield. The CFD results show that the overall performance of M-Busemann intake has a good aerodynamic achievement, with a total pressure recovery reaching a very high value of 0.55. The influence of the calorically perfect model and thermally perfect model on the performance of the intake is not particularly obvious.

AB - The detailed design steps and the idea of connecting M-flow and truncated Busemann flow are given in this paper. A new improved method is proposed to effectively reduce the size of the expansion zone in the original parent flowfield. The database of MBus parent flowfield at free-stream Mach 4 and Mach 6 is provided. Finally, a Mach-6 M-Busemann intake is designed to verify the performance of the improved parent flowfield. The CFD results show that the overall performance of M-Busemann intake has a good aerodynamic achievement, with a total pressure recovery reaching a very high value of 0.55. The influence of the calorically perfect model and thermally perfect model on the performance of the intake is not particularly obvious.

KW - Busemann flow

KW - Hypersonic

KW - Streamline tracing

KW - Wavecatcher intake

UR - https://www.scopus.com/pages/publications/85123629120

U2 - 10.1016/j.ast.2022.107376

DO - 10.1016/j.ast.2022.107376

M3 - 文章

AN - SCOPUS:85123629120

SN - 1270-9638

VL - 121

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

M1 - 107376

ER -

Flow quality in an M-Busemann wavecatcher intake

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Keywords

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