Consistent Boundary Conditions for Multicomponent Real Gas Mixtures Based on Characteristic Waves

By N. Okong'o, J. Bellan. 2002

169 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/dda71ee5df304195250fcc9162bfb4a410b8c39b

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Chun Sang Yoo
2. Hong G. Im
3. E. Taşkinoğlu
4. T. Schmitt
5. Laurent Selle
6. Bénédicte Cuenot
7. A. Trouvé
8. Yang Wang

In Applied Mathematics

1. Hong G. Im
2. Chun Sang Yoo
3. E. Taşkinoğlu
4. T. Schmitt
5. Laurent Selle
6. A. Trouvé
7. Yang Wang
8. Anthony Ruiz

In Computational Mechanics

1. Chun Sang Yoo
2. E. Taşkinoğlu
3. Hong G. Im
4. T. Schmitt
5. Bénédicte Cuenot
6. Laurent Selle
7. Anthony Ruiz
8. A. Trouvé

Citations in the corpus

• A posteriori study using a DNS database describing fluid disintegration and binary-species mixing under supercritical pressure: heptane and nitrogen (2010, methodology): “These HDGM regions were found in both pre-transitional (Miller et al. 2001) and transitional (Okong’o & Bellan 2002b; Okong’o, Harstad & Bellan 2002) temporal mixing layers and were shown to arise from the combined effect of the distortion of the initial density boundary and of mixing (Okong’o &…”
• Improved boundary conditions for viscous, reacting, compressible flows (2003, unknown): “Keywords: Reacting flows; Boundary conditions; Navier–Stokes; Characteristic; Flame–boundary interaction”
• Characteristic boundary conditions for simulations of compressible reacting flows with multi-dimensional, viscous and reaction effects (2007, methodology): “The NSCBC approach was further extended to consider multi-component reacting flows [13, 14], and subsonic nonreflecting inflow conditions were also derived as a variation within the generalized formulation [15].”
• Large-Eddy Simulation of Supercritical-Pressure Round Jets (2010, methodology): “Finally, the boundary conditions are treated with the characteristic wave decomposition method NSCBC (Navier–Stokes characteristic boundary conditions) [41,47], which was also adapted to real-gas thermodynamics [48].”
• Characteristic boundary conditions for direct simulations of turbulent counterflow flames (2005, methodology): “Further recent developments of NSCBC include an adaptation to multi-component chemically reacting flows [17, 18], a modified treatment of the chemical reaction source terms at the domain boundaries [19], and a low Mach number asymptotic expansion to decouple acoustics from other flow variables for s”