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J-GLOBAL ID:200902289744779466   Reference number:04A0159690

Mixing of a Hydrogen Jet from a Wedge Shaped Injector into a Supersonic Cross Flow

くさび形状インジェクタからの超音速直交流に対する水素噴流の混合
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Volume: 46  Issue: 154  Page: 217-223  Publication year: Feb. 04, 2004 
JST Material Number: F0167A  ISSN: 0549-3811  CODEN: TJASA  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: ENGLISH (EN)
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Gas turbines 
Reference (17):
  • 1) Scuderi, L. F., Orton, G. F. and Hunt, J. L.: Mach 10 Cruise/Space Access Vehicle Definition, AIAA Paper 98-1584, In AIAA Space Planes and Hypersonic Systems and Technologies Conference, 1998.
  • 2) Sunami, T.: Breakdown Process of Supersonic Streamwise Vortices in Spanwise-Row Configuration, Nagare, J. Jpn. Soc. Fluid Mech., 18 (1999), pp. 136–139 (in Japanese).
  • 3) Wilson, M. P., Bowersox, R. D. W. and Glawe, D. D.: Experimental Investigation of the Role of Downstream Ramps on a Supersonic Injection Plume, J. Propul. Power, 15 (1999), pp. 432–439.
  • 4) Morita, S., Arai, T., Nagata, H., Hosokawa, H. and Sugiyama, H.: Enhancement of Supersonic Mixing by Backward Facing Step with Ramp Partially (Evaluation of Mixing Condition Using Catalytic Reaction on Constant Temperature Pt Wire), Proceedings of the 38th Conference on Aerospace Propulsion and the 8th Symposium on RAM/SCRAMJETS, 1998, pp. 33–35 (in Japanese).
  • 5) Gruber, M. R., Nejad, A. S., Chen, T. H. and Dutton, J. C.: Mixing and Penetration Studies of Sonic Jets in a Mach 2 Freestream, J. Propul. Power, 11 (1995), pp. 315–323.
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