Shock stand-off distances over sharp wedges for thermally non-equilibrium dissociating nitrogen flows

Author:

Yildiz U.ORCID,Vatansever D.ORCID,Celik B.ORCID

Funder

National Centre of High-Performance Computing of Turkey

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Engineering,Condensed Matter Physics,Computational Mechanics

Reference42 articles.

1. Hermann, R.: Hypersonic non-equilibrium flow and its thermodynamic relations. Technical Report, No. UARI-30, NASA https://ntrs.nasa.gov/api/citations/19660012369/downloads/19660012369.pdf (1965). Accessed 26 November 2022

2. Vatansever, D., Celik, B.: Unsteady shock interaction mechanisms of high enthalpy reacting flows over double wedges at Mach 7. Phys. Fluids 33(4), 056110 (2021). https://doi.org/10.1063/5.0050202

3. Anderson, J.D.: Hypersonic and High Temperature Gas Dynamics, 2nd ed, AIAA Education Series. AIAA, Reston, VA, USA (2006). https://doi.org/10.2514/4.861956

4. Candler, G.V., MacCormack, R.W.: Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium. J. Thermophys. Heat Transf. 5(2), 266–273 (1991). https://doi.org/10.2514/3.260

5. Kumar, S., Olivier, H.: Numerical simulation of chemically reactive hypersonic flows. PhD Dissertation, No. RWTH-CONV-122682, Fakultät für Maschinenwesen https://publications.rwth-aachen.de/record/60997/files/Kumar_Sanjeev.pdf (2006). Accessed 26 November 2022

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