Sources of Turbulence on an Unswept Wing of a Supersonic Passenger Airplane

被引：2
作者：
Chuvakhov P.V. [1 ,2 ]
Pogorelov I.O. [1 ,2 ]
机构：
[1] Moscow Institute of Physics and Technology (MIPT), Moscow
[2] Zhukovsky Central Aerohydrodynamic Institute, Moscow oblast, Zhukovsky
来源：
Mathematical Models and Computer Simulations | 2023年 / 15卷 / 2期
基金：
俄罗斯科学基金会;
关键词：
acoustic noise; atmospheric turbulence; laminarization; numerical simulation; sources of turbulence; SPA; supersonic passenger airplane; unswept wing;
D O I：
10.1134/S2070048223020035
中图分类号：
学科分类号：
摘要：
Abstract: The two most likely sources of disturbances capable of triggering boundary layer turbulization over a smooth unswept wing of a supersonic airplane are considered in terms of the full Navier–Stokes equations: atmospheric turbulence and acoustic noise radiated by the turbulent boundary layer over the fuselage. The frequency wave characteristics of boundary layer disturbances over the wing are analyzed and the dominant mechanism of transition is revealed. The numerical results are compared with those of linear stability theory. © 2023, Pleiades Publishing, Ltd.
引用
收藏
页码：177 / 188
页数：11
相关论文
共 21 条
  • [1] Liebhardt B., Lutjens K., Tracy R.R., Haas A.O., Exploring the prospect of small supersonic airliners – A business case study based on the Aerion AS2 jet, In 17Th AIAA Aviation Technology, Integration, and Operations Conference, pp. 2017-3588, (2017)
  • [2] Reshotko E., Boundary-layer stability and transition, Annu. Rev. Fluid Mech., 8, pp. 311-349, (1976)
  • [3] Notes on initial disturbance fields for the transition problem, In Instability and Transition, pp. 217-232, (1990)
  • [4] Zhigulev V.N., Fedorov A.V., Boundary-layer receptivity to acoustic disturbances, J. Appl. Mech. Tech. Phys., 28, pp. 28-34, (1987)
  • [5] Fedorov A.V., “Receptivity of hypersonic boundary layer to acoustic disturbances scattered by surface roughness, In 33Rd AIAA Fluid Dynamics Conference and Exhibit, pp. 2003-3731, (2003)
  • [6] Turco R.P., Upper-atmosphere aerosols: Properties and natural cycles, The Atmospheric Effects of Stratospheric Aircraft: A First Program Report, NASA RP-1272, 3B, pp. 63-91, (1992)
  • [7] Pugach M.A., Ryzhov A.A., Fedorov A.V., Estimation of the effect of free-stream turbulence and solid particles on the laminar–turbulent transition at hypersonic speeds, TsAGI Sci. J., 47, 1, pp. 15-28, (2016)
  • [8] Fedorov A.V., Receptivity of a supersonic boundary layer to solid particulates, J. Fluid Mech., 737, pp. 105-131, (2013)
  • [9] Chuvakhov P.V., Fedorov A.V., Obraz A.O., Numerical modelling of supersonic boundary-layer receptivity to solid particulates, J. Fluid Mech., 859, pp. 949-971, (2019)
  • [10] Egorov I.V., Fedorov A.V., Novikov A.V., Chuvakhov P.V., The role of receptivity in prediction of high-speed laminar-turbulent transition, IUTAM Laminar-Turbulent Transition, Proc. IUTAM Symposium, London, UK, 38, pp. 541-552, (2019)
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