Introduction
While flying with hypersonic speed, the aircraft vehicle will produce very strong shock wave. The interactions between shock wave and boundary layer not only increase the drag, but also produce high pressure and high aerodynamic heating. The shock wave oscillation usually appears in the inlet of engine and in the flow inside the high-speed turbine, and this phenomena can cause unsteady heating, and excite various kinds of unsteady modes to result in tired material destroy. Therefore, it is very essential to strengthen the study and set up the effective estimate or prediction method of shock wave and boundary layer interactions.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsPreview
Unable to display preview. Download preview PDF.
References
Transition in wall-bounded flows. Applied Mechanics Reviews 61, 030802-1 (2008)
Lee, C., Wu, J.: Transition in wall-bounded flows. Advances in Mechanics 39(4) (2009)
Poggie, J., Erbland, P.J., Smits, A.J., Miles, R.B.: Quantitative visualization of compressible turbulent shear flows using condensate-enhanced Rayleigh scattering, Experiments in Fluids. Experimental Methods and their Applications to Fluid Flow (2004)
Greene, B.G.: Major, USMC: Characterization and control of carbon dioxide seed particles in image velocimetry. AFIT/GAE/ENY/08-M12, Air Force Institute of Technology (2008)
Zhao, Y.X., Yi, S.H., Tian, L.F., et al.: Supersonic flow imaging via nanoparticles. Sci. China Ser. E-Tech. Sci. 52(12), 3640–3648 (2009)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2012 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Li, M., Yi, Sh., Zhu, Zw., He, L. (2012). Application of NPLS Technique to Hypersonic Shock-Wave and Boundary Layer Interactions. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25688-2_96
Download citation
DOI: https://doi.org/10.1007/978-3-642-25688-2_96
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-25687-5
Online ISBN: 978-3-642-25688-2
eBook Packages: EngineeringEngineering (R0)