Global measurements of hypersonic shock-wave/boundary-layer interactions with pressure-sensitive paint

Author:

Running Carson L.ORCID,Juliano Thomas J.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference89 articles.

1. Anderson J (2006) Hypersonic and high temperature gas dynamics, chap 7, 2nd edn. American Institute of Aeronautics and Astronautics Inc., Reston

2. Arnal D, Délery J (2005) Laminar-turbulent transition and shock wave/boundary layer interaction. Technical Report 116, RTO-EN-AVT

3. Asma C, Paris S, Tapsoba M (2002) Transitional shock-wave boundary layer interaction over a cone-flare model at hypersonic conditions. ESASP Paper 487

4. Babinsky H, Harvey J (2011) Shock wave-boundary-layer interactions. Cambridge University Press, New York

5. Baccarella D, Liu Q, Passaro A, Lee T, Do H (2016) Development and testing of the ACT-1 experimental facility for hypersonic combustion research. Meas Sci Technol 27:4

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