Hypersonic entry heating with discontinuous surface Catalycity: A combined analytic/CFD approach

Theroretical Fluid Mechanics Conference

Volumn , Issue , 1996, Pages

  Inger, George R ^a,c   Gnoffo, Peter A ^b,d  

^a IOWA STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Dept of Aerospace Engr and Engr Mechanics ^*  (United States)

^d Aerothermodynamics Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLUID DYNAMICS; FLUID MECHANICS; INTERFACES (MATERIALS); NAVIER STOKES EQUATIONS;

ANALYTICAL METHOD; CATALYCITY; CATALYTIC EFFICIENCIES; DISCONTINUOUS SURFACES; FINITE SURFACE; NAVIER STOKES; POST PROCESSING; THERMAL PROTECTION MATERIAL;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84983175113     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Ihger, G. R., “Nonequilibrium Boundary Layer Effects on the Aerodynamic Heating of Hypersonic Waverider Vehicles,” Journal of Thermosphysics and Heat Transfer. Vol. 20, No. 10, January-February 1996, pp. 20.
2. Hayes, W. D. and R. F. Probstein, Hypersonic Row Theory. Academic Press, NY, 1959, p. 293-312.
3. Inger, G. R., “Dissociated Laminar Boundary Layer Flows over Surfaces with Arbitrary Continuous Distributions of Catalycity,” Int. J. Heat and Mass Tiaasfcl, & Sept 1963, pp. 815-832.
4. Inger, G. R., “Nonequilibrium Stagnation Point Boundary Layers with Arbitrary Surface Catalycity,” A1AA Journal. Vol. 1, No. 8, August 1963, pp. 1776-1781.
5. Gnoffo, P. A., “An Upwind-Biased, Point-Implicit Relaxation Algorithm for Viscous, Compressible Perfect-Gas Hows,” NASA TP 2953, February 1990.
6. Stewart, D. A., Leiser, D. B., Kolodziej, P., and Smith, M., “Thermal Response of Integral Multicomponent Composite Thermal Protection Systems,” AIAA Paper 85-1056, June 1985.