Exploratory RANS and LES simulations of transient supersonic combustor flow

Author:

Ebrahimi Houshang1,Gaitonde Datta2,Malo-Molina Faure2

Affiliation:

1. Software and Engineering Associates, Inc.

2. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. 1Curran,E.andMurthy,S.“ScramjetPropulsion,”ProgressinAeronauticsandAstronauticsSeries,Vol.V-189,2001.

2. 2Walker,S.,Rodgers,F.,andEsposita,A.“HypersonicCollaborativeAustralia/UnitedStatesExperiment(HYCAUSE),”AIAAPaper2005-3254, 2005.

3. 3Billig, F. and Jacobsen, L. “Comparison of Planar and Axisymmetric Flowpaths for Hydrogen Fueled Space Access Vehicles (Invited),” AIAAPaper2003-4407,2003.

4. 4Drayna,T.,Nompelis,I.,andCandler,G.“HypersonicInwardTurningInlets: DesignandOptimization,”AIAAPaper2006-297,Jan.2006.

5. 5Ungewitter,R.,Ott,J.,andDash,S.“AdvancedModelingMethodsforHypersonicScramjetEvaluation,”AIAAPaper2006-4578,2006.

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