Conceptual Study into Wave Ingesting Propulsion for Hypersonic Flight
Paper
Paper/Presentation Title | Conceptual Study into Wave Ingesting Propulsion for Hypersonic Flight |
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Presentation Type | Paper |
Authors | Jahn, Ingo H. |
Journal or Proceedings Title | Proceedings of the 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference |
Article Number | 3034 |
Number of Pages | 16 |
Year | 2023 |
Place of Publication | United States |
ISBN | 9781624107108 |
Digital Object Identifier (DOI) | https://doi.org/10.2514/6.2023-3034 |
Web Address (URL) of Paper | https://arc.aiaa.org/doi/abs/10.2514/6.2023-3034 |
Web Address (URL) of Conference Proceedings | https://arc.aiaa.org/doi/book/10.2514/MHYP23 |
Conference/Event | 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference |
Event Details | 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference Parent AIAA International Space Planes and Hypersonic Systems and Technologies Conference Delivery In person Event Date 28 May 2023 to end of 01 Jun 2023 Event Location Bengaluru, Karnataka, India |
Abstract | Boundary layer or wake ingesting propulsion systems are gaining increased attention in the design of sub-sonic flight vehicles. They deliver performance gains by re-energising drag processed flow. The high speed flight analogy are wave ingesting propulsion systems, that attempt to manipulate the movement of momentum in order to minimise or eliminate drag. |
Contains Sensitive Content | Does not contain sensitive content |
ANZSRC Field of Research 2020 | 4001. Aerospace engineering |
Public Notes | Files associated with this item cannot be displayed due to copyright restrictions. |
Byline Affiliations | University of Southern Queensland |
https://research.usq.edu.au/item/z213y/conceptual-study-into-wave-ingesting-propulsion-for-hypersonic-flight
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