Study of the Influence of the Temperature Field’s Nonuniformity on the Pressure Pulsations in the Inlet Duct Using the RANS/ILES Method

Author:

Ayupov R. S.,Benderskiy L. A.,Lyubimov D. A.

Publisher

Pleiades Publishing Ltd

Subject

Computational Mathematics,Modeling and Simulation

Reference15 articles.

1. Flow investigations in a stalling nacelle inlet under disturbed inflow;S. Übelacker,2016

2. J. M. Abbott, “Computational study of the aerodynamic performance of subsonic scarf inlets,” in Proceedings 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 11–14,2004, Fort Lauderdale, FL, AIAA Paper 2004-3406.

3. Y. Colina, B. Aupoixb, J. F. Boussugea, and P. Chanez, “Numerical simulation and analysis of crosswind inlet flows at low Mach numbers,” in Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Interior Flows,2007, ISAIF8-0058.

4. Simulation of interaction of aircraft with gust and resolved LES-simulated atmospheric turbulence;P. Kelleners,2016

5. U. R. Oriji, X. Yang, and P. G. Tucker, “Hybrid RANS/ILES for aero engine intake,” in Proceedings of ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, June 16–20,2014, Dusseldorf, Germany, GT2014-26472.

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