Study of the RANS / ILES flow method in a high-speed mixed-air inlet for various operating modes

 
PIIS004036440002714-9-1
DOI10.31857/S004036440002714-9
Publication type Article
Status Published
Authors
Affiliation: FSUE Central Institute of Aviation Motors P.I. Baranova
Address: Russian Federation
Affiliation: FSUE Central Institute of Aviation Motors P.I. Baranova
Address: Russian Federation
Journal nameTeplofizika vysokikh temperatur
EditionVolume 56 Issue 5
Pages729-737
Abstract

  

Keywords
AcknowledgmentРабота выполнена при частичной поддержке гранта РФФ И (№ 15–08–01996-A).
Received27.12.2018
Publication date27.12.2018
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1. Tan H.-J., Sun S., Yin Z.-L. Oscillatory Flows of Rectangular Hypersonic Inlet Unstart Causrd by Dounstream Mass-Flow Choking // J. Prop. Power. 2009. V. 25. № 1. P. 138.

2. Li Z., Gao W., Jiang H., Yang J. Unsteady Behaviors of a Hypersonic Inlet Caused by Throttling in Shock Tunnel // AIAA J. 2013. V. 51. № 10. P. 2485.

3. Peterson D.M., Candler G. V., Drayna T. W. Detached Eddy Simulation of a Generic Scramjet Inlet and Combustor // AIAA Paper 2009–130. 2009.

4. You Y., Luedeke H., Hannemann K. Injection and Mixing in a Scramjet Combustor: DES and RANS Studies // Proc. Combust. Inst. 2013. V. 34. P. 2083.

5. Trapier S., Deck S., Duveau P. Delayed Detached-Eddy Simulation and Analysis of Supersonic Inlet Buzz // AIAA J. 2008. V. 46. № 1. P. 118.

6. Peterson D.M., Boyce R. R., Wheatley V. Simulations of Mixing in an Inlet-Fueled Axisymmetric Scramjet // AIAA J. 2013. V. 51. № 12. P. 2823.

7. Shur M.L., Spalart P. R., Strelets M. K., Travin A. K. A Hybrid RANS-LES Approach with Delayed-DES and Wall-modeled LES Capabilities // Int. J. Heat Fluid Flow. 2008. V. 29. P. 1638.

8. Boles J.A ., Choi J.-I., Edwa rd s J . R . , Baurle R. A. Simulations of High-Speed Internal Flows using LES/RANS Models // AIAA Paper 2009–1324. 2009.

9. Lyubimov D.A., Potekhina I. V. Issledovanie nestatsionarnykh rezhimov raboty sverkhzvukovogo vozdukhozabornika RANS/ILES-metodom // TVT. 2016. T. 54. № 5. S. 784.

10. Lyubimov D. A. Chislennoe issledovanie nestatsionarnykh turbulentnykh techenij v sverkhzvukovykh diffuzorakh // XI Vseros. s'ezd po fundament. problemam teor. i prikl. mekhaniki. Kazan', 2015. S. 2399. CD.

11. Spa l a r t P. R . , Jou W. -H., St rel ets M., Allmaras S. R. Comments on the Feasibility of LES for Wings, and on a Hybrid RANS/LES Approach // 1st AFOSR Int. Conf. on DNS/LES. Rouston, Louisiana, USA, 1997. P. 669.

12. Yan J., Tawackolian K., Michel U., Thiele F. Computation of Jet Noise using a Hybrid Approach // AIAA Paper 2007–3621. 2007.

13. Islam A., Thornber B. A Hybrid RANS-Implicit LES Method for External Aerodynamics // Proc. 19th Australasian Fluid Mechanics Conf. Melbourne. Australia. 8–11 Dec. 2014.

14. Wei Q., Chen H.-X., Ma Z. A Hybrid RANS/LES Model for Simulation of Complex Turbulent Flow // J. Hydrodyn. 2016. V. 28. № 5. P. 811.

15. Nakamori I., Ikohagi T. Dynamic Hybridization of MILES and RANS for Predicting Airfoil Stall // Comput. Fluids. 2008. V. 37. P. 161.

16. Morgan P.E., Visbal M. R. Application of Hybrid RANS/ ILES to Geometries with Separated Flows // AIAA Paper 2006–3028. 2006.

17. Zhu H., Fu S., Lei Shi L., Wang Z. J. A Hybrid RANSImplicit LES Approach for the High-Order FR/CPR Method // AIAA Paper 2016–1599. 2016.

18. Spalart P.R., Deck S., Shur M. L., Squires K. D., Strelets M. K., Travin A. A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities // Theor. Comput. Fluid Dyn. 2006. V. 20. P. 181.

19. Lyubimov D. A. Razrabotka i primenenie ehffektivnogo RANS/ILES-metoda dlya rascheta slozhnykh turbulentnykh struj // TVT. 2008. T. 46. № 2. S. 271.

20. Lyubimov D. A. Razrabotka i primenenie metoda vysokogo razresheniya dlya rascheta strujnykh techenij metodom modelirovaniya krupnykh vikhrej // TVT. 2012. T. 50. № 3. S. 450.

21. Suresh A., Huynh H. T. Accurate Monotonicity – Preserving Schemes with Runge–Kutta Time Stepping // J. Comput. Phys. 1997. V. 136. № 1. P. 83.

22. Spalart P.R., Allmaras S. R. A One-Equation Turbulence Model for Aerodynamic Flows // La Recherche Aerospatiale. 1994. № 1. P. 5.

23. Vogel J.C., Eaton J. K. Combined Heat Transfer and Fluid Dynamic Measurements Downstream of a Backward-facing Step // J. Heat Mass Transfer (Trans. ASME). 1985. V. 107. P. 922.

24. Stepanov V.A., Makarov A. Yu., Maslov V. P. Experimental Study of Synthetic Jets for the Control of Flows Separation in the Engine’s Ducts // 29th Int. Congress of the Aeronautical Science. St.-Petersburg. Russia. Sept. 7–12. 2014. Paper № 280.

25. Lyubimov D.A., Potekhina I. V. Primenenie RANS/ILES-metoda dlya analiza ehffektivnosti upravleniya otryvnymi techeniyami v diffuzorakh s pomosch'yu sinteticheskikh struj // Izv. RAN. MZhG. 2015. № 4. S. 144.

26. Lyubimov D., Makarov A., Potekhina I. Experimental and Numerical Research of Unsteady Flow in Curvilinear Channel with Active Flow Management using «Synthetic» Jets // 28th Int. Congress of the Aeronautical Science. Brisbane. Australia. Sept. 23–28. 2012.

27. Sun P.Z., Shi H. T., Lu X. Y. Numerical Investigation of the Unsteady Behavior of a Hypersonic Inlet under Throttling // Procedia Eng. 2015. V. 126. P. 179.

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