Hydrogen-oxygen induction times above crossover temperatures

被引:62
作者
Del Alamo, G
Williams, FA [1 ]
Sánchez, AL
机构
[1] Univ Calif San Diego, Dept Mech & Aerosp Engn, La Jolla, CA 92093 USA
[2] Univ Carlos III Madrid, Escuela Politecn Super, Area Mecan Fluidos, Madrid, Spain
关键词
hydrogen-oxygen ignition times; crossover temperatures; short mechanism; analytical induction time; asymptotic analysis;
D O I
10.1080/00102200490487175
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ignition in hydrogen-oxygen systems above crossover temperatures and under various conditions of pressure and composition is addressed computationally and by asymptotic methods. Different descriptions of the detailed chemistry are evaluated through comparison of computed and measured ignition times, and a balance between accuracy and simplicity is struck in selecting rate parameters to be used in investigating reduced chemistry. Through numerical calculations for isobaric, homogeneous, and adiabatic hydrogen-air mixtures it is shown that the detailed chemistry can be reduced to only six elementary steps for determining induction times over the range of conditions addressed. From these six steps, an analytical expression for ignition time is derived which agrees well with computational results concerning dependence on pressure, temperature, and composition. It is shown that O and OH maintain steady states during ignition for stoichiometric and fuel-rich mixtures, whereas H maintains, a steady state for sufficiently fuel-lean conditions. Simple asymptotic formulas for the induction times are derived for these two limits that demonstrate the limiting effect of O-2 under rich conditions and of H-2 under lean conditions. These formulas are combined in an approximate way to obtain an expression for the ignition time that can be used for all equivalence ratios.
引用
收藏
页码:1599 / 1626
页数:28
相关论文
共 48 条
[1]   High pressure studies of moist carbon monoxide nitrous oxide kinetics [J].
Allen, MT ;
Yetter, RA ;
Dryer, FL .
COMBUSTION AND FLAME, 1997, 109 (03) :449-470
[2]  
ASABA T, 1965, P COMBUST INST, V10, P295
[3]   TURBULENT COMBUSTION REGIMES FOR HYPERSONIC PROPULSION EMPLOYING HYDROGEN-AIR DIFFUSION FLAMES [J].
BALAKRISHNAN, G ;
WILLIAMS, FA .
JOURNAL OF PROPULSION AND POWER, 1994, 10 (03) :434-437
[4]  
Belles FE, 1965, P COMBUST INST, V10, P285
[5]   SHOCK-TUBE STUDY OF EFFECT OF UNSYMMETRIC DIMETHYL HYDRAZINE ON IGNITION CHARACTERISTICS OF HYDROGEN-AIR MIXTURES [J].
BHASKARAN, KA ;
GUPTA, MC ;
JUST, T .
COMBUSTION AND FLAME, 1973, 21 (01) :45-48
[6]   Optimally-reduced kinetic models: reaction elimination in large-scale kinetic mechanisms [J].
Bhattacharjee, B ;
Schwer, DA ;
Barton, PI ;
Green, WH .
COMBUSTION AND FLAME, 2003, 135 (03) :191-208
[7]  
Blumenthal R., 1996, Proc 20th ISSW World Scientific, V2, P935
[8]  
CHENG RK, 1977, THESIS U CALIFORNIA
[9]  
COHEN A, 1967, 1386 BRL US ARM
[10]  
Craig R. R., 1966, AFAPLTR6674