Apparent Subsonic Choking in Dual-Stream Nozzles
Author:
Affiliation:
1. ASTECH, Meudon-la-Foret, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61406
Reference6 articles.
1. Interaction between primary and secondary streams of supersonic ejector systems and their performance characteristics
2. Compound-Compressible Nozzle Flow
3. Choked flow - A generalization of the concept and some experimental data.
Cited by 6 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. Study on the compressible viscous flows through a straight pipe;Journal of Mechanical Science and Technology;2011-02
2. Analysis of Choked Viscous Flows through a Constant Area Duct;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2010-05-14
3. Propagation of weak pressure waves against two parallel subsonic streams;Journal of Thermal Science;2006-06
4. Compound choking of a two-parallel stream through a convergent duct;KSME International Journal;2001-12
5. Blockierungs-Kriterium für den Sekundärstrom eines Überschall-Ejektors mit zylindrischer Mischkammer;Forschung im Ingenieurwesen;1996-03
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