Influence of Nozzle Exit Conditions on the Near-Field Development of High Subsonic and Underexpanded Axisymmetric Jets

Author:

Trumper Miles,Behrouzi Parviz,McGuirk James

Funder

EPSRC

Publisher

MDPI AG

Subject

Aerospace Engineering

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Simulation of supersonic jet flow past a blunt body in a laboratory experiment using computer vision;Acta Astronautica;2024-02

2. Application of a wide-range nozzle with a central body in ultralight launch vehicles;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

3. Propulsive jet aerodynamics and aeroacoustics;The Aeronautical Journal;2021-11-19

4. The near-field aerodynamic characteristics of hot high-speed jets;Journal of Fluid Mechanics;2021-03-29

5. Aspect Ratio Driven Relationship between Nozzle Internal Flow and Supersonic Jet Mixing;Aerospace;2021-03-16

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