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Volumn 11, Issue 1, 1997, Pages 36-44

Different levels of modeling for diffusion phenomena in neutral and ionized mixtures

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; ELECTRIC FIELD EFFECTS; FLOW OF FLUIDS; IONIZATION OF GASES; MATHEMATICAL MODELS; MAXWELL EQUATIONS; MIXTURES; PRESSURE EFFECTS; REYNOLDS NUMBER; SPECIFIC HEAT; THERMAL CONDUCTIVITY; THERMAL EFFECTS;

EID: 0030735738     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6220     Document Type: Article
Times cited : (8)

References (16)
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    • Blottner, F.G.1
  • 4
    • 0014639565 scopus 로고
    • Viscous Shock Layer at the Stagnation Point with Nonequilibrium Air Chemistry
    • Blottner, F. G., "Viscous Shock Layer at the Stagnation Point with Nonequilibrium Air Chemistry," AIAA Journal, Vol. 7, No. 12, 1969, pp. 2281-2288.
    • (1969) AIAA Journal , vol.7 , Issue.12 , pp. 2281-2288
    • Blottner, F.G.1
  • 5
    • 16444381040 scopus 로고
    • A Unified Approximation for the Mixture Transport Properties for Multicomponent Boundary Layer Applications
    • Feb.
    • Kendal, R. M., Rindall, R. A., and Bartlett, E. P., "A Unified Approximation for the Mixture Transport Properties for Multicomponent Boundary Layer Applications," NASA CR 1063, Feb. 1968.
    • (1968) NASA CR 1063
    • Kendal, R.M.1    Rindall, R.A.2    Bartlett, E.P.3
  • 6
    • 85006932360 scopus 로고
    • A Multicomponent Boundary Layer Chemically Coupled to Ablating Surface
    • Kendal, R. M., Rindall, R. A., and Bartlett, E. P., "A Multicomponent Boundary Layer Chemically Coupled to Ablating Surface," AIAA Journal, Vol. 5, No. 6, 1967, pp. 1063-1071.
    • (1967) AIAA Journal , vol.5 , Issue.6 , pp. 1063-1071
    • Kendal, R.M.1    Rindall, R.A.2    Bartlett, E.P.3
  • 7
    • 85006933917 scopus 로고
    • An Extension of the Roe Approximate Riemann Solver for the Approximation of Navier-Stokes Equations in Chemical Nonequilibrium Cases
    • Nova Science Publishers, New York
    • Dubroca, B., and Gallice, G., "An Extension of the Roe Approximate Riemann Solver for the Approximation of Navier-Stokes Equations in Chemical Nonequilibrium Cases," Computing Methods in Applied Sciences and Engineering, Nova Science Publishers, New York, 1991.
    • (1991) Computing Methods in Applied Sciences and Engineering
    • Dubroca, B.1    Gallice, G.2
  • 9
    • 0342585267 scopus 로고
    • Chemical Kinetics of High Temperature Air
    • edited by F. Ridell, Academic
    • Wray, K. L., "Chemical Kinetics of High Temperature Air," Hypersonic Flow Research, edited by F. Ridell, Academic, 1962, pp. 181-204.
    • (1962) Hypersonic Flow Research , pp. 181-204
    • Wray, K.L.1
  • 10
    • 7044275089 scopus 로고
    • Nonequilibrium Effects for Hypersonic Transitional Flows
    • Jan.
    • Moss, J. N., Cuda, V., and Simmonds, A. L., "Nonequilibrium Effects for Hypersonic Transitional Flows." AIAA Paper 87-0404, Jan. 1987.
    • (1987) AIAA Paper 87-0404
    • Moss, J.N.1    Cuda, V.2    Simmonds, A.L.3
  • 13
    • 85006324774 scopus 로고
    • Re-Entry Flight Predictions Around a Hyperboloid-Flare by Means of Non-Equilibrium Real Gas Navier-Stokes Simulation
    • June
    • Durand, G., Coron, F., Drouin, N., Duffa, G., Desmeuzes, C., Devezeaux, D., and Hughes, E., "Re-Entry Flight Predictions Around a Hyperboloid-Flare by Means of Non-Equilibrium Real Gas Navier-Stokes Simulation," AIAA Paper 94-1824, June 1994.
    • (1994) AIAA Paper 94-1824
    • Durand, G.1    Coron, F.2    Drouin, N.3    Duffa, G.4    Desmeuzes, C.5    Devezeaux, D.6    Hughes, E.7
  • 14
    • 0014580568 scopus 로고
    • Role of Charge Separation and Pressure Diffusion in the Gascap of Entry Objects
    • Howe, J. T., and Sheaffer, Y. S., "Role of Charge Separation and Pressure Diffusion in the Gascap of Entry Objects," AIAA Journal, Vol. 7, No. 10, 1969, pp. 1971-1977.
    • (1969) AIAA Journal , vol.7 , Issue.10 , pp. 1971-1977
    • Howe, J.T.1    Sheaffer, Y.S.2
  • 15
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    • Transport Coefficients Determined Using the Shielded Coulomb Potential
    • Liboff, R. L., "Transport Coefficients Determined Using the Shielded Coulomb Potential," Physics of Fluids, Vol. 2, No. 1, 1959, pp. 40-46.
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  • 16
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    • Finite Rate Plasma Generation in the Laminar Air Boundary Layer on Slender Re-Entry Bodies
    • San Diego, CA
    • Blottner, F. G., and Lenard, M., "Finite Rate Plasma Generation in the Laminar Air Boundary Layer on Slender Re-Entry Bodies," 8th Symposium on Ballistic Missile and Space Technology, San Diego, CA, 1963.
    • (1963) 8th Symposium on Ballistic Missile and Space Technology
    • Blottner, F.G.1    Lenard, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.