Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection
Oblique detonation wave (ODW) reflection on the upper wall leads to a sophisticated wave complex, whose stability is critical to the application of oblique detonation engines. The unstable wave complex characterized with a continuous moving Mach stem has been observed, but the corresponding re-stabi...
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doaj-8a707cfd6de046b193cab59af3f9a9a32021-07-23T14:03:22ZengMDPI AGProcesses2227-97172021-07-0191215121510.3390/pr9071215Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave ReflectionAifeng Wang0Jiahao Shang1Qiu Wang2Kuanliang Wang3Aero Engine Academy of China, Aero Engine Corporation of China, Beijing 101304, ChinaState Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, ChinaState Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, ChinaSchool of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, ChinaOblique detonation wave (ODW) reflection on the upper wall leads to a sophisticated wave complex, whose stability is critical to the application of oblique detonation engines. The unstable wave complex characterized with a continuous moving Mach stem has been observed, but the corresponding re-stability adjusting method is still unclear so far. In this study, the cowl-induced expansion wave based on the model with an upper-side expansion wall is introduced, and the ODW dynamics have been analyzed using the reactive Euler equations with a two-step induction–reaction kinetic model. With the addition of a cowl-induced expansion wave, the re-stabilized Mach stem has been distinguished. This re-stability is determined by the weakened secondary reflection wave of lower wall, while the final location of Mach stem is not sensitive to the position of the expansion corner. The re-stabilized ODW structure is also basically irrelevant to the expansion angle, while it may shift to unstable due to the merging of subsonic zones. Transient phenomena for the unstable state have been also discussed, clarifying fine wave structures further.https://www.mdpi.com/2227-9717/9/7/1215oblique detonationasymmetricnozzlereflection |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Aifeng Wang Jiahao Shang Qiu Wang Kuanliang Wang |
spellingShingle |
Aifeng Wang Jiahao Shang Qiu Wang Kuanliang Wang Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection Processes oblique detonation asymmetric nozzle reflection |
author_facet |
Aifeng Wang Jiahao Shang Qiu Wang Kuanliang Wang |
author_sort |
Aifeng Wang |
title |
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection |
title_short |
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection |
title_full |
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection |
title_fullStr |
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection |
title_full_unstemmed |
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection |
title_sort |
effects of cowl-induced expansion on the wave complex induced by oblique detonation wave reflection |
publisher |
MDPI AG |
series |
Processes |
issn |
2227-9717 |
publishDate |
2021-07-01 |
description |
Oblique detonation wave (ODW) reflection on the upper wall leads to a sophisticated wave complex, whose stability is critical to the application of oblique detonation engines. The unstable wave complex characterized with a continuous moving Mach stem has been observed, but the corresponding re-stability adjusting method is still unclear so far. In this study, the cowl-induced expansion wave based on the model with an upper-side expansion wall is introduced, and the ODW dynamics have been analyzed using the reactive Euler equations with a two-step induction–reaction kinetic model. With the addition of a cowl-induced expansion wave, the re-stabilized Mach stem has been distinguished. This re-stability is determined by the weakened secondary reflection wave of lower wall, while the final location of Mach stem is not sensitive to the position of the expansion corner. The re-stabilized ODW structure is also basically irrelevant to the expansion angle, while it may shift to unstable due to the merging of subsonic zones. Transient phenomena for the unstable state have been also discussed, clarifying fine wave structures further. |
topic |
oblique detonation asymmetric nozzle reflection |
url |
https://www.mdpi.com/2227-9717/9/7/1215 |
work_keys_str_mv |
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_version_ |
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