Computational combustion simulation for an aircraft model combustor-Reference-Cited by-同舟云学术

Computational combustion simulation for an aircraft model combustor

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
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Author:

Kunz O.¹,Noll B.¹,Lueckerath R.¹,Aigner M.¹,Hohmann S.²

Affiliation:

1. DLR, German Aerospace Center, Stuttgart, Germany

2. Muenchen, Technische Hochschule, Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3706

Reference14 articles.

1. Hassa, C., Carl, M., Frodermann, M., Behrendt, T.,Heinze,J., Fleing, C., Meier, U., Wolff-GaBmann, D., Hohmann, S., Zarzalis, N., 2000, "Experimental and Numerical Investigation of a Planar Combustor Sector at Realistic Conditions", ASMEpaper 2000-GT-0123

2. Meier, U.E., Wolff-GaBmann, D., Stricker, W., 2000, "LIF Imaging and 2D Temperature Mapping in a Model Combustor atElevated Pressure", Aerospace Science and Technology, inpress

3. Luckerath, R., Bergmann, V., Stricker, W., 1998, "Characterization of gas turbine combustion chambers with single pulse CARS thermometry", AGARD-CP-598

4. Fluent User's Guide, 1998, Fluent Inc., Lebanon,USA

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