Experimental methods of exhaust nozzle in ramjet engines
Document Type
Article
Publication Date
12-1-2010
Abstract
A new method for the exhaust nozzle of the hypersonic ramjet in ground tests has been developed in this paper. The high enthalpy gas was produced steadily in double detonation driven shock tube to simulate the condition of the ramjet at high Mach number. And a new method to calculate the thrust with pilot pipe was given according to the law of conservation of momentum. All these provided foundation for catalysis compound experiment.
Publication Source (Journal or Book title)
Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
First Page
621
Last Page
625
Recommended Citation
Li, B., Li, J., Yu, H., & Chen, H. (2010). Experimental methods of exhaust nozzle in ramjet engines. Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 28 (6), 621-625. Retrieved from https://repository.lsu.edu/ag_exst_pubs/514