199937th Aerospace Sciences Meeting and ExhibitRequires access

The effect of entrance conditions on an expanding arcjet flow

Joseph Sheeley, Maurice Holt, Mark Loomis

Open publisher page 1 citations

Abstract

Flow development with various entrance conditions in a conical arcjet nozzle is simulated for a test gas consisting of nitrogen and argon. Simulations with uniform nozzle entrance conditions are performed and nozzle exit centerline conditions are compared with available experimental data. Simulations with entrance conditions consisting of a hot core and cooler annulus are then performed, and it is found that the non-uniformity persists through the nozzle, affecting the exit centerline temperature and velocity. Pitot pressure and heat transfer profiles determined horn simulated exit conditions are used to evaluate the effectiveness of pitot pressure and calorimeter measurements in determining the extent of flow uniformity. It is found that heat transfer measurements are far superior to pitot pressure measurements in assessing flow uniformity.

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What this paper is about

Flow development with various entrance conditions in a conical arcjet nozzle is simulated for a test gas consisting of nitrogen and argon. Simulations with uniform nozzle entrance conditions are performed and nozzle exit centerline conditions are compared with available experimental data. Simulations with entrance conditions consisting of a hot core and cooler annulus are then performed, and it is found that the non-uniformity persists through the nozzle, affecting the exit centerline temperature and velocity. Pitot pressure and heat transfer profiles determined horn simulated exit conditions are used to evaluate the effectiveness of pitot pressure and calorimeter measurements in determining the extent of flow uniformity. It is found that heat transfer measurements are far superior to pitot pressure measurements in assessing flow uniformity.

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Available abstract

Flow development with various entrance conditions in a conical arcjet nozzle is simulated for a test gas consisting of nitrogen and argon. Simulations with uniform nozzle entrance conditions are performed and nozzle exit centerline conditions are compared with available experimental data. Simulations with entrance conditions consisting of a hot core and cooler annulus are then performed, and it is found that the non-uniformity persists through the nozzle, affecting the exit centerline temperature and velocity. Pitot pressure and heat transfer profiles determined horn simulated exit conditions are used to evaluate the effectiveness of pitot pressure and calorimeter measurements in determining the extent of flow uniformity. It is found that heat transfer measurements are far superior to pitot pressure measurements in assessing flow uniformity.

Key concepts: Pitot tube, Nozzle, Arcjet rocket, Mechanics, Materials science, Heat transfer, Flow (mathematics), Conical surface

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