Skip to main content
Log in

Receptivity of hypersonic boundary layer due to fast-slow acoustics interaction

  • Research Paper
  • Published:
Acta Mechanica Sinica Aims and scope Submit manuscript

Abstract

The objective of receptivity is to investigate the mechanisms by which external disturbances generate unstable waves. In hypersonic boundary layers, a new receptivity process is revealed, which is that fast and slow acoustics through nonlinear interaction can excite the second mode near the lower-branch of the second mode. They can generate a sum-frequency disturbance though nonlinear interaction, which can excite the second mode. This receptivity process is generated by the nonlinear interaction and the nonparallel nature of the boundary layer. The receptivity coefficient is sensitive to the wavenumber difference between the sum-frequency disturbance and the lower-branch second mode. When the wavenumber difference is zero, the receptivity coefficient is maximum. The receptivity coefficient decreases with the increase of the wavenumber difference. It is also found that the evolution of the sum-frequency disturbance grows linearly in the beginning. It indicates that the forced term generated by the sum-frequency disturbance resonates with the second mode.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16

Similar content being viewed by others

References

  1. Kachanov, Y.S.: Physical mechanisms of laminar-boundary layer transition. Annu. Rev. Fluid Mech. 26, 411–482 (1994)

    Article  MathSciNet  Google Scholar 

  2. Ma, Y.B., Zhong, X.L.: Receptivity of a supersonic boundary layer over a flat plate, part 1. Wave structures and interactions. J. Fluid Mech. 488, 31–78 (2003)

    Article  MathSciNet  MATH  Google Scholar 

  3. Brandt, L., Schlatter, P., Henningson, D.S.: Transition in boundary layers subject to free-stream turbulence. J. Fluid Mech. 517, 167–198 (2004)

    Article  MathSciNet  MATH  Google Scholar 

  4. Fedorov, A.V.: Transition and stability of high-speed boundary layers. Annu. Rev. Fluid Mech. 43, 79–95 (2011)

    Article  Google Scholar 

  5. Zhong, X.L., Wang, X.W.: Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers. Annu. Rev. Fluid Mech. 44, 527–561 (2012)

    Article  MathSciNet  Google Scholar 

  6. Fedorov, A.V.: Receptivity of a high-speed boundary layer to acoustic disturbances. J. Fluid Mech. 491, 101–129 (2003)

    Article  MATH  Google Scholar 

  7. Goldstein, M.E.: The evolution of Tollmien–Schlichting waves near a leading edge. J. Fluid Mech. 127, 59–81 (1983)

    Article  MathSciNet  MATH  Google Scholar 

  8. Goldstein, M.E.: Scattering of acoustic waves into Tollmein–Schichting waves by small streamwise variation in surface geometry. J Fluid Mech. 154, 509–529 (1985)

    Article  MATH  Google Scholar 

  9. Choudhari, M., Streett, C.: A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions. Phys. Fluids 4, 2495–2514 (1992)

    Article  MATH  Google Scholar 

  10. Fedorov, A.V., Khokhlov, A.P.: Excitation of unstable modes in a supersonic boundary layer by acoustic waves. Fluid Dyn. 9, 456–467 (1991)

  11. Fedorov, A.V.: Prehistory of instability in a hypersonic boundary layer. Theor. Comput. Fluid Dyn. 14, 359–375 (2001)

    Article  MATH  Google Scholar 

  12. Fedorov, A.V.: Receptivity of a high-speed boundary layer to acoustic disturbance. J. Fluid Mech. 491, 101–129 (2003)

    Article  MATH  Google Scholar 

  13. Ma, Y.B., Zhong, X.L.: Receptivity of a supersonic boundary layer over a flat plate, part 2. Receptivity to free-stream sound. J. Fluid Mech. 488, 79–121 (2003)

    Article  MathSciNet  MATH  Google Scholar 

  14. Ma, Y.B., Zhong, X.L.: Receptivity of a supersonic boundary layer over a flat plate, part 3. Effects of different types of free-stream disturbances. J. Fluid Mech. 532, 63–109 (2005)

    Article  MathSciNet  MATH  Google Scholar 

  15. Balakumar, P.: Receptivity of a supersonic boundary to acoustic disturbances. AIAA J. 47, 1069–1078 (2009)

    Article  Google Scholar 

  16. Luo, J.S., Zhou, H.: On the generation of Tollmien–Schlichting waves in the boundary layer of a flat plate by disturbances in the free stream. Proc. R. Soc. Lond. 416, 351–367 (1987)

    Article  Google Scholar 

  17. Wu, X.S.: Generation of Tollmien–Schlichting waves by convecting gusts interacting with sound. J. Fluid Mech. 397, 285–316 (1999)

    Article  MATH  Google Scholar 

  18. Saric, W.S., Reed, H.L., Kerschen, E.J.: Boundary-layer receptivity to freestream disturbance. Annu. Rev. Fluid Mech. 34, 291–319 (2002)

  19. Zhang, H., Luo, J.S.: Computation of perturbation equations in compressible boundary layer. J. Yanshan Univ. 31, 248–252 (2007)

    Google Scholar 

  20. Poinsot, T.J., Lele, S.K.: Boundary condition for direct simulations of compressible viscous flows. J. Comput. Phys. 101, 104–129 (1992)

    Article  MathSciNet  MATH  Google Scholar 

  21. Gaydos, P., Tumin, A.: Multimode decomposition in compressible boundary layers. AIAA J. 42, 1115–1121 (2004)

    Article  Google Scholar 

  22. Gao, J., Luo, J.S.: Mode decomposition of nonlinear eigenvalue problems and application in flow stability. Appl. Math. Mech. 35, 667–674 (2014)

    Article  MathSciNet  MATH  Google Scholar 

  23. Balakumar, P., Malik, M.R.: Discrete modes and continuous spectra in supersonic boundary layer. J. Fluid Mech. 239, 631–656 (1992)

    Article  MATH  Google Scholar 

  24. Tumin, A.: Three-dimensional spatial normal modes in compressible boundary layers. J. Fluid Mech. 586, 295–322 (2007)

    Article  MathSciNet  MATH  Google Scholar 

Download references

Acknowledgments

The project was supported by the National Natural Science Foundation of China (Grants 11332007 and 11202147) and the Specialized Research Fund for the Doctoral Program of Higher Education (Grants 20120032120007).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Ji-Sheng Luo.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Gao, J., Luo, JS. & Wu, XS. Receptivity of hypersonic boundary layer due to fast-slow acoustics interaction. Acta Mech. Sin. 31, 899–909 (2015). https://doi.org/10.1007/s10409-015-0504-8

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10409-015-0504-8

Keywords

Navigation