Observations on using experimental data as boundary conditions for computations

AIAA Journal

Volumn 33, Issue 1, 1995, Pages 176-178

  Orkwis, Paul D ^a   Tam, Chung Jen ^a   Disimile, Peter J ^a  

^a UNIVERSITY OF CINCINNATI   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALCULATIONS; MATHEMATICAL MODELS; PRANDTL NUMBER; REYNOLDS NUMBER; SHOCK WAVES; TURBULENCE; WIND TUNNELS;

ADIABATIC WALL CONDITIONS; COMPUTATIONAL EFFORTS; COMPUTATIONAL GRID POINTS; CROCCO BUSEMANN RELATION; LENGTH TO DEPTH RATIO; MACH NUMBER; NONDIMENSIONAL FLOW FIELDS PARAMETER; TWO DIMENSIONAL FLOW;

BOUNDARY CONDITIONS;

EID: 0029219099     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.12355     Document Type: Article

References (4)

1. Hankey, W. L., and Shang, J. S., “Analysis of Pressure Oscillations in an Open Cavity,” AIAA Journal, Vol. 18, No. 8, 1980, pp. 892-898.
2. Rizzetta, D. P., “Numerical Simulation of Supersonic Flows over a Three Dimensional Cavity,” AIAA Journal, Vol. 26, No. 7, 1988, pp. 799-807.
3. Baysal, O., Fouladi, K., Leung, R. W., and Sheftic, J. S., “Interference Flows Past Cylinder-Fin-Sting-Cavity Assemblies,” Journal of Aircraft, Vol. 29, No. 2, 1992, pp. 194-202.
4. Dusing, D. W., Fox, C. W., Tam, C.-J., Orkwis, P. D., and Disimile, P. J., “An Experimental and Computational Study of Unsteady Supersonic 2-D Open Cavity Flow Physics,” AIAA Paper 94-0589, Jan. 1994.