Development of Single and Multi-jet Conical Nozzle Based Open Jet Facility for Cold Jet Simulation

Author:

Sunny Kalakanda Alfred,Kumar Nallapaneni Manoj,Justin Aldin,Harithra M.

Publisher

Springer Singapore

Reference17 articles.

1. Jayahar Sivasubramanian and Hermann F. Fasel.: Numerical Investigation of Shockwave Boundary Layer Interactions in Supersonic Flows. 54th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, (AIAA 2016-0613), pp. 1–42. < http://dx.doi.org/10.2514/6.2016-0613 >.

2. S. Pirozzoli, J. Larsson, J. W. Nichols, M. Bernardini, B. E. Morgan, S. K. Lele.: Analysis of unsteady effects in shock/boundary layer interactions. Proceedings of the Summer Program 2010, Center for Turbulence Research, pp. 153–164, (2010).

3. Green, J. E.: Interactions between shock waves and turbulent boundary layers. Progress in Aerospace Sciences, Vol. 11, pp. 235–340, December (1970).

4. Rose W. C., M. E. Childs.: Reynolds-shear-stress measurements in a compressible boundary layer within a shock-wave-induced adverse pressure gradient. Journal of Fluid Mechanics, Vol. 65, Issue. 01, pp. 177–188, August (1974).

5. Babinsky Holger, John K. Harvey.: Shock wave boundary layer interactions. Vol. 32. Cambridge University Press, (2011).

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