Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench

Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench

For studies of hypersonic flows and supersonic combustion in ground test facilities, three devices can be used as ram accelerators, shock tunnels and supersonic combustor test benches. These devices can reproduce, on the ground, similar conditions to those in real flight at a certain altitude and s...

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Bibliographic Details
Main Authors: Jefte da Silva Guimarães, Valéria Serrano Faillace Oliveira Leite, Dermeval Carinhana Junior, Marco Antônio Sala Minucci
Format: Article
Language:English
Published: Departamento de Ciência e Tecnologia Aeroespacial 2020-10-01
Series:Journal of Aerospace Technology and Management
Subjects:
scramjet
supersonic flow
ground testing facilities
supersonic nozzle
schlieren technique
Online Access:https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e4820.pdf

Internet

https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e4820.pdf

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