Quasi-one-dimensional modeling of hydrogen fuelled scramjet combustors

Collection of Technical Papers - 18th AIAA Computational Fluid Dynamics Conference

Volumn 2, Issue , 2007, Pages 1325-1337

  Birzer, Cristian ^a,b   Doolan, Con J ^a,b,c  

^a UNIVERSITY OF ADELAIDE   (Australia)

^b School of Mechanical Engineering

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HYDROGEN FUELLED SCRAMJET; OPEN THERMODYNAMIC SYSTEMS; SCRAMJET PROPULSION; SUPERSONIC COMBUSTION;

COMBUSTORS; GAS DYNAMICS; HEAT TRANSFER; MATHEMATICAL MODELS; ORDINARY DIFFERENTIAL EQUATIONS; RUNGE KUTTA METHODS; SYSTEMS ANALYSIS;

RAMJET ENGINES;

EID: 35648934965     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Smart, M.K., Hass, N.E. and Paull, A. "Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment", AIAA Journal, Vol. 4, No. 10, 2006, pp 2375-2366.
2. Moses, P.L., Rausch, V.L., Nguyen, L.T. and Hill, J.R. "NASA Hypersonic Flight Demonstrators - Overview, Status and Future Plans", Acta Astronautica, Vol. 55, 2004, pp. 619-630.
3. O'Brien, T., Starkey, R. and Lewis, M. "Quasi-One-Dimensional High-Speed Engine Model with Finite Rate Chemistry", Journal of Propulsion and Power, Vol. 17, No. 6, 2001, pp. 1366-1374.
4. Starkey, R. P. and Lewis, M. J. "Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic Missile Design," Journal ofPropulsion and Power, Vol. 19, No. 1, 2003, pp. 89-97.
5. Shapiro, A. The Dynamics and Thermodynamics of Compressible Fluid Flow, Vol. 1, Ronald, New York, 1953.
6. Anderson, J.D. Hypersonic and High Temperature Gas Dynamics, AIAA, Reston, VA, USA, 2000.
7. Turns, S.R. An Introduction to Combustion, McGraw Hill, New York, 1996.
8. Gordon, S. and McBride, B.J. "Computer program for calculation of complex chemical equilibrium compositions, rocket performance, incident and reflected shocks, and Chapman-Jouguet detonations", NASA Special Publication, NASA SP-273, 1976.
9. Borman, G.L. and Ragland, K.W. Combustion Engineering, McGraw Hill, Boston, 1998.
10. Morley, C. GasEq, Version 0.79 http://www.gaseq.co.uk, 2005.
11. Driscoll, J.F., Huh, H., Yoon, Y. and Donbar, J. "Measured Lengths of Supersonic Hydrogen-Air Jet Flames - Compared to Subsonic Flame Lengths - and Analysis", Combustion and Flame, Vol. 107, pp. 76-186, 1996.
12. Papamoschou, D. and Roshko, A. "The Compressible Turbulent Shear Layer: An Experimental Study", Journal of Fluid Mechanics, Vol. 197, pp. 453-477, 1988.
13. Gerlinger, P. and Bruggemann, D. "Numerical Investigation of Hydrogen Strut Injections into Supersonic Airflows", Journal of Propulsion and Power, Vol. 16, No. 1, pp. 22-28, 2000.
14. Boyce, R.R., Paull, A., Stalker, RJ., Wendt, M., Chinzei, N. and Miyajima, H. "Comparison of Supersonic Combustion Between Impulse and Vitiation-Heated Facilities", Journal of Propulsion and Power, Vol. 16, No. 4, pp. 709-717, 2000.
15. Goyne, C.P., McDaniel, J. C., Quagliaroli, T.C., Krauss, R.H. and Day, S. W. "Dual -Mode Combustion of Hydrogen in a Mach 5, Continuous-Flow Facility", Journal of Propulsion and Power, Vol. 17, No. 6, pp 1313-1318, 2001.