SIMULATION OF FLOW SEPARATION IN TURBOJET ENGINE INLETS

Author:

Engulatova M. F.,Liverko D. V.,Lysenkov A. V.,Matyash S. V.,Savelyev A. A.

Publisher

Pleiades Publishing Ltd

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference14 articles.

1. D. L. Daggett, “Ultra Efficient Engine Technology Systems Integration and Environmental Assessment," NASA Langley Res. Cent., No, 7, 1–54 (2002).

2. K. S. Anisimov, A. A. Savelyev, I. A. Kursakov, et al., “Propulsion System — Airframe Integration and Optimization of Civil Aircraft — Agile EU Project," in Proc. of the 31st Congr. Intern. Count. Aeronaut. Sci. ICAS 2018, Belo Horizonte (Brazil), 9–14 Sept. 2018. S. l.: S. n., 2018.

3. A. I. Troshin, “Comparison of Modern Differential Models for Reynolds Stresses in Turbulent-Boundary Layer Separation Problems," in Proc. 12th All- Russian Congress on Fundamental Problems of Theoretical and Applied Mechanics, Ufa (Russia), 19–24 Aug. 2019 (Bashkir State Univ., Ufa, 2019), 699–700.

4. M. L. Shur, P. R. Spalart, M. K. Strelets, and A. V. Garbaruk, “Further Steps in LES-Based Noise Prediction for Complex Jets," in Proc. of the 44th AIAA Aerospace Sciences Meeting and Exhibit., Reno (USA), 9–12 Jan. 2006. S. l.: AIAA, 8, 5784–5809 (2006).

5. Aerodynamics, Stability, and Controllability of Supersonic Aircraft, Ed. by G. S. Byushgens (Nauka, Moscow, 1988).

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