Thrust enhancement in hypervelocity nozzles by chemical catalysis

Journal of Propulsion and Power

Volumn 13, Issue 4, 1997, Pages 574-576

  Singh, D J ^a,c   Carpenter, Mark H ^b   Drummond, J P ^b  

^a ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c JACOBS TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; CATALYSIS; HYPERSONIC FLOW; MATHEMATICAL MODELS; NOZZLES;

EULER CODE; PHOSPHINE; RUNGE-KUTTA METHOD; THRUST ENHANCEMENT;

RAMJET ENGINES;

EID: 0031188477     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.5206     Document Type: Article

References (3)

1. Menees, G. P., Adelman, H. G., Gambier, J.-L., and Bowles, J. V., "Wave Combustors for Trans-Atmospheric Vehicles," Journal of Propulsion and Power, Vol. 8, No. 3, 1992, pp. 709-713.
2. Twarowski, A., "The Influence of Phosphorus Oxides and Acids on the Rate of H + OH Recombination," Combustion and Flame, Vol. 94, Nos. 1/2, 1993, pp. 91-107.
3. Twarowski, A., "The Effect of Phosphorus Chemistry on Recombination Losses in a Supersonic Nozzle," Combustion and Flame, Vol. 102, Nos. 1/2, 1995, pp. 55-63.