Combustion Study of the Boron Particles in the Secondary Chamber of Ducted Rocket
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Publisher
American Institute of Aeronautics and Astronautics
Reference10 articles.
1. Flow measurements in a model ramjet secondary combustion chamber
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3. An LES for the Effects of Particle Size and Velocity Ratio on the Flow Structure in the Secondary Combustor;International Journal of Aeronautical and Space Sciences;2020-07-20
4. Effect of tangential swirl air inlet angle on the combustion efficiency of a hybrid powder-solid ramjet;Acta Astronautica;2019-06
5. Experimental Investigation of a Solid Propellant Ducted Rocket with a Chin Type Inlet;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2019
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