Displacement effects and scaling of ducted, supersonic flames

Combustion and Flame

Volumn 116, Issue 4, 1999, Pages 593-604

  Wendt, M N ^a   Jacobs, P A ^a   Stalker, R J ^a  

^a UNIVERSITY OF QUEENSLAND   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; DENSITY OF GASES; ENTHALPY; FUEL INJECTION; HYDROGEN; PRESSURE DISTRIBUTION; REDUCTION; SHOCK WAVES; SUPERSONIC FLOW; TURBULENT FLOW; WALL FLOW;

FREE-PISTON SHOCK TUNNELS; LUDWIEG TUNNELS; SUPERSONIC HYDROGEN-AIR FLAMES;

FLAME RESEARCH;

HYDROGEN;

AIR; FLAME; HYDROGEN; SUPERSONIC FLOW;

ARTICLE; COMBUSTION; ENTHALPY; FIRE; PRESSURE; PRIORITY JOURNAL; SHOCK WAVE;

EID: 0033103132     PISSN: 00102180     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0010-2180(98)00069-8     Document Type: Article

References (18)

1. G. Y. Anderson, A. Kumar, and J. Erdos. Progress in hypersonic combustion technology with computation and experiment. AIAA Paper 90-5254, 1990.
2. R. G. Morgan and R. J. Stalker. Hypersonic combustion of hydrogen in a shock tunnel. In Ninth International Symposium on Air Breathing Engines, Athens, Greece, p. 577-584, 1989.
3. P. A. Jacobs, R. G. Morgan, R. C. Rogers, M. Wendt, C. Brescianini, A. Paull, and G. Kelly. Preliminary calibration of a generic scramjet combustor. Department of Mechanical Engineering Report, University of Queensland, 1990.
4. M. Wendt. Supersonic combustion with hot hydrogen injection. PhD thesis, The University of Queensland, Brisbane, Australia, February 1994.
5. Brescianini C.P., Morgan R.G. Numerical modeling of wall-injected scramjet models. A.I.A.A. J. Propulsion Power. 9:1993;169-175.
6. R. J. Stalker and R. G. Morgan. The University of Queensland free piston shock tunnel T4: Initial operation and preliminary calibration. In Fourth National Space Symposium, Adelaide, 1988.
7. M. K. McIntosh. Computer program for the numerical calculation of frozen and equilibrium conditions in shock tunnels. Department of Physics Unpublished Technical Report, Australian National University, Canberra, 1968.
8. J. A. Lordi, R. E. Mates, and J. R. Moselle. Computer program for the numerical solution of non-equilibrium expansions of reacting gas mixtures. NASA Contractor Report 472, 1965.
9. D. J. Mee. Uncertainty analysis of conditions in the test section of the T4 shock tunnel. Department of Mechanical Engineering Research Report 4/93, The University of Queensland, Brisbane, 1993.
10. Morgan R.G., Stalker R.J. Fast acting hydrogen valve. J. Phys. E. Sci. Instr. 16:1983;205-207.
11. K. A. Skinner. Mass spectrometry in shock tunnel experiments of hypersonic combustion. PhD thesis, The University of Queensland, Brisbane, Australia, 1994.
12. Evans J.S., Schexnayder C.J. Jr. Influence of chemical kinetics and unmixedness on burning in supersonic hydrogen flames. A.I.A.A. J. 18:1980;188-193.
13. Launder B.E., Spalding D.B. The numerical computation of turbulent flows. Computer Methods Appl. Mech. Engineering. 3:1974;269-289.
14. Brescianini C.P. Modified k-ε model for compressible free shear flows. A.I.A.A. J. 30:(8):1992;2161-2163.
15. Buttsworth D.R., Morgan R.G. Shock-tunnel investigation of hypervelocity free shear layers in a planar duct. A.I.A.A. J. Propulsion Power. 12:1996;998-1000.
16. Stalker R.J., Morgan R.G. Supersonic hydrogen combustion with a short thrust nozzle. Combust. Flame. 57:1984;55-70.
17. Hermanson J.C., Mungal M.G., Dimotakis P.E. Heat release effects on shear-layer growth and entrainment. A.I.A.A. J. 25:1987;578-583.
18. Anderson J.D. Hypersonic and High Temperature Gas Dynamics. 1989;McGraw-Hill, New York.