Testing of solid fuel ramjet with measurement of thrust characteristics in aerodynamic facilities View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

2018-07

AUTHORS

D. A. Vnuchkov, V. I. Zvegintsev, D. G. Nalivaichenko, V. I. Smolyaga, A. V. Stepanov

ABSTRACT

A design of an axisymmetric solid fuel ramjet consisting of a multi wedges nose air intake, solid fuel gas gene-rator, combustion chamber, and a nozzle, was developed. According to this design, a ramjet model for tests in the ground wind-tunnel facilities was fabricated. Experiments with solid fuel combustion were carried out in the Transit-M and T-313 wind tunnels, ITAM SB RAS, at air-flow Mach numbers М = 2.5−5.0. High values of the internal and net excess thrust were obtained. More... »

PAGES

605-611

Identifiers

URI

http://scigraph.springernature.com/pub.10.1134/s0869864318040121

DOI

http://dx.doi.org/10.1134/s0869864318040121

DIMENSIONS

https://app.dimensions.ai/details/publication/pub.1110717096


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