Numerical Investigation of a 3-D Chemically Reacting Scramjet Engine at High Altitudes Using JP8

Numerical Investigation of a 3-D Chemically Reacting Scramjet Engine at High Altitudes Using JP8 - Air Mixtures

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Malo-Molina Faure¹,Gaitonde Datta¹,Ebrahimi Houshang²

Affiliation:

1. Computational Sciences Branch

2. Aerospace Testing Alliance

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1435

Reference29 articles.

1. Gaitonde, Datta V. "Three Dimensional Flow-Through Scramjet Simulation with MHD Energy-Bypass," AIAA Paper 2003-0172, January2003.

2. Gruber, M. R., Jackson, K., Mathur, T., and Billig, F. "Experiments with a Cavity-Based Fuel Injector for Scramjet Applications," InternationalSocietyofAir-BreathingEngines,ISABE PaperIS-7154,Sept.1999.

3. Baurle, R. A.,Tam, C.J., and Dasgupta, S. "Analysis of Unsteady Cavity Flows for Scramjet Applications," AIAA Paper 2000-3617,July2000.

4. Effect of Flame-Holding Cavities on Supersonic-Combustion Performance

5. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

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