Analysis of a Multi-Porthole Injector Array in a Supersonic Crossflow
Author:
Affiliation:
1. RMIT University, Melbourne, Victoria 3053, Australia
2. Bundeswehr University Munich, 85579 Neubiberg, Germany
3. University of Queensland, Brisbane, Queensland 4072, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference30 articles.
1. Characteristics of Dual Transverse Injection in Scramjet Combustor, Part 1: Mixing
2. The influence of micro air jets on mixing augmentation of transverse hydrogen jet in supersonic flow
3. Supersonic Boundary-Layer Combustion via Multiporthole Injector Arrays
4. Experimental investigation of flame-holding capability of hydrogen transverse jet in supersonic cross-flow
5. Detailed flow physics of the supersonic jet interaction flow field
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