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

This document is currently not available here.

Share

COinS