Title of article :
Numerical Study on the Effect of Jet on the Operation of Powder Fuel Scramjet
Author/Authors :
Ding, H . m School of Mechanical and Engineering - Nanjing University of Science and Technology Nanjing 210094 - China , Zhuo, , C .f School of Mechanical and Engineering - Nanjing University of Science and Technology Nanjing 210094 - China , Hu, , W .G Yibin North Chuan’an Chemical Industry Co - Ltd - Sichuan 644219 - China , Deng, H.Y School of Mechanical and Engineering - Nanjing University of Science and Technology Nanjing 210094 - China , Chen, X School of Mechanical and Engineering - Nanjing University of Science and Technology Nanjing 210094 - China
Abstract :
Metal powder fuel ha s high energy and volume calorific value s, and it is an excellent power fuel for hypersonic aircraft in the future . However, metal powder ha s poor flow characteristics and is difficult to be effectively mixed with air when supersonic air is injected . The mixing degree of fuel and air is an important factor to the efficiency of the engine. One way to solve this problem is to introduce a jet ( t he primary jet) upstream of the
powder fuel inlet to improve the mixing degree of fuel and increase the residence time. In this study, a double
hole jet two dimensional scramjet combustor structure w as established, the effects of different initial jet
conditions on the performance of scramjets was studied and analyzed. The results show that the introduction of
the primary jet can effectively improve t he mixing degree of the powder ed fuel and air in the combustion
chamber p rolong the residence time of the particles in the combustion chamber and improves the combustion
efficiency of the metal powder. However, both the combustion efficiency of the metal powder fuel and engine thrust increase and then decrease when the mass flow rate of the primary jet increases.
Keywords :
Scramjet , Numerical simulation , Powder fuel , Jet , Combustion efficiency
Journal title :
Journal of Applied Fluid Mechanics (JAFM)