Design of heated flow wind tunnel facility for testing small size ramjet engine combustors
This report documents the research studies on the design of a 'high speed heated flow wind tunnel facility', to test a 'Trapped Vortex Concept' (TVC) combustor of a ramjet engine, designed for the DSO National Laboratories, Singapore. The ramjet is to operate at flight s...
Main Author: | Panikulam, John Paul |
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Other Authors: | Randy Chue |
Format: | Thesis |
Language: | English |
Published: |
2015
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Subjects: | |
Online Access: | http://hdl.handle.net/10356/65089 |
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