2000Journal of Propulsion TechnologyOpen access

Measurement and analysis for shock due to the secondary gas injection

Lai Chuan

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Abstract

Research for bow shock due to secondary gas injection was developed with different points of injection,Mach numbers and jet angles Experiments were carried out in two dimensional rectangular jet for photos taken with Schlieren apparatus The experimental data obtained from Schlieren photograph were compared with the results calculated from the blast wave theory It proved that the shock radium solutions from the blast wave agreement with the experiments

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Research for bow shock due to secondary gas injection was developed with different points of injection,Mach numbers and jet angles Experiments were carried out in two dimensional rectangular jet for photos taken with Schlieren apparatus The experimental data obtained from Schlieren photograph were compared with the results calculated from the blast wave theory It proved that the shock radium solutions from the blast wave agreement with the experiments

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Available abstract

Research for bow shock due to secondary gas injection was developed with different points of injection,Mach numbers and jet angles Experiments were carried out in two dimensional rectangular jet for photos taken with Schlieren apparatus The experimental data obtained from Schlieren photograph were compared with the results calculated from the blast wave theory It proved that the shock radium solutions from the blast wave agreement with the experiments

Key concepts: Schlieren, Schlieren imaging, Mach number, Shock wave, Blast wave, Jet (fluid), Shock diamond, Shock (circulatory)

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