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Near-field shock/shear-layer interactions in a two-stream supersonic rectangular jet from three-stream engine
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[1] Kan, Pinqing
[2] Ruscher, Christopher J.
[3] Lewalle, Jacques
[4] Gogineni, Sivaram
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1600年
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AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States卷
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56期
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This work would not have been possible without many sponsors and access to computational resources. The LES data were produced using the Naval Research Laboratory JENRE code and the authors are thankful for the advice from NRL scientists (Kamal Viswanath and Kailas Kailasnath) on the computational work. The simulations shown in this paper were performed on Garnet;
one of the DoD supercomputing resource centers operated by the high-performance computing modernization program. Pinqing Kan was supported by Syracuse University. Christopher Ruscher was supported by an SBIR Phase II and Phase I funding with AFRL Turbine Engine Division. Jacques Lewalle was supported in part by the SBIR Phase I funding for AFRL;
in part by an AFOSR grant (No. FA9550-15-1-0435) under the direction of R. Ponnappan. We also greatly benefited from the interactions with the Glauser Group at Syracuse University;
and the members of the Air Force noise team (Barry Kiel;
Alex Giese;
and Thomas Ferril);
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