TY - GEN
T1 - Effect of injector variation on the bidirectional vortex
AU - Maicke, Brian A.
AU - Talamantes, Gerardo
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2016
Y1 - 2016
N2 - The primary goal of this work is to assess the sensitivity of the bidirectional vortex to changes in injection conditions. To achieve this goal, a parametric model is developed to capture the effect of variations in number of injectors, injector size, injection velocity, and injection location. The resulting cold-flow model is simulated using OpenFOAM, an open source platform for the solution of fluid dynamics problems. The accuracy of the solver is validated through comparisons to existing analytical models. After the validation is complete, simulations are run to examine the response of the vortex to changes in the injector design. The resulting axial and velocity profiles are be compared to evaluate the sensitivity of the vortex structure to the injection conditions. It is found that increasing mass flow rate by way of injector number, injector size, and injection velocity all have an amplifying effect on the peak velocities in all directions. Changes in the injection height have a nominal effect on the swirl and radial velocities, but a more significant impact on the axial velocity.
AB - The primary goal of this work is to assess the sensitivity of the bidirectional vortex to changes in injection conditions. To achieve this goal, a parametric model is developed to capture the effect of variations in number of injectors, injector size, injection velocity, and injection location. The resulting cold-flow model is simulated using OpenFOAM, an open source platform for the solution of fluid dynamics problems. The accuracy of the solver is validated through comparisons to existing analytical models. After the validation is complete, simulations are run to examine the response of the vortex to changes in the injector design. The resulting axial and velocity profiles are be compared to evaluate the sensitivity of the vortex structure to the injection conditions. It is found that increasing mass flow rate by way of injector number, injector size, and injection velocity all have an amplifying effect on the peak velocities in all directions. Changes in the injection height have a nominal effect on the swirl and radial velocities, but a more significant impact on the axial velocity.
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U2 - 10.2514/6.2016-4581
DO - 10.2514/6.2016-4581
M3 - Conference contribution
AN - SCOPUS:85059960259
SN - 9781624104060
T3 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
BT - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Y2 - 25 July 2016 through 27 July 2016
ER -