科研之友
微信
新浪微博
Facebook
分享链接
摘要
A comprehensive analysis of the efficiency of an approach based on the injection of a thin oxygen stream, subjected to a tailored electric discharge, into a supersonic H-2-air flow to enhance the combustion performance in the mixing layer and in the scramjet combustor is conducted. It is shown that for such an approach there exist optimal values of reduced electric field E/N and transversal dimension d of the injected oxygen stream, which provide the minimal length of induction zone in the mixing layer. The optimal values of E/N and d depend on air flow parameters and the specific energy put into the oxygen. The injection of a thin oxygen stream (d = 1 mm) subjected to an electric discharge with E/N = 50-100 Td, which produces mostly singlet oxygen O-2(a(1) Delta(g)) and O-2(b(1) Sigma(+)(g)) molecules and atomic oxygen, allows one to arrange stable combustion in a scramjet duct at an extremely low air temperature T-air = 900 K and pressure P-air = 0.3 bar even at a small specific energy put into the oxygen E-s = 0.2 J nc m(-3), and to provide rather high combustion completeness eta = 0.73. The advance in the energy released during combustion is much higher (hundred times), in this case, than the energy supplied to the oxygen stream in the electric discharge. This approach also makes it possible to ensure the rather high combustion completeness in the scramjet combustor with reduced length. The main reason for the combustion enhancement of the H-2-air mixture in the scramjet duct is the intensification of chain-branching reactions due to the injection of a small amount of cold non-equilibrium oxygen plasma comprising highly reactive species, O-2(a(1) Delta(g)) and O-2(b(1) Sigma(+)(g)) molecules and O atoms, into the H-2-air supersonic flow.
- 出版日期2013-12
