Apparatus to produce high-temperature gas for simulating hypersonic propulsion

Document Type

Article

Publication Date

12-1-2009

Abstract

In an effort to increase the thrust of scramjet engines at high Mach numbers, a method was developed to produce high-temperature gas for catalysis. Theoretical analyses and numerical calculations were conducted and a shock tunnel to produce mixtures of high-temperature air and gas-fuel was built. Reproducible results were obtained at 3200 K and a total pressure of 2 MPa. The experimental time approached 17 ms.

Publication Source (Journal or Book title)

Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica

First Page

34

Last Page

39

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