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NASA NTRS · 20190000380

CFD Simulations for Arc-Jet Panel Testing Capability Development Using Semi-Elliptical Nozzles

Gokcen, Tahir·Balboni, John A.·Hartman, Grover J.
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Abstract

This paper reports computational simulations in support of arc-jet panel testing capability development using semi-elliptical nozzles in a high enthalpy arc-jet facility at NASA Ames Research Center. Two different semi-elliptical nozzle configurations are proposed for testing panel test articles. Computational fluid dynamics simulations are performed to provide estimates of achievable panel surface conditions and useful test area for each configuration. The present analysis comprises three-dimensional simulations of the nonequilibrium flowfields in the semi-elliptical nozzles, test box and flowfield over the panel test articles. Computations show that useful test areas for the proposed two nozzle options are 20.32 centimeters by 20.32 centimeters (8 inches by 8 inches) and 43.18 centimeters by 43.18 centimeters (17 inches by 17 inches). Estimated values of the maximum cold-wall heat flux and surface pressure are 155 watts per centimeters squared and 39 kilopascals for the smaller panel test option, and 44 watts per centimeters squared and 7 kilopascals for the larger panel test option. Other important properties of the predicted flowfields are presented, and factors that limit the useful test area in the semi-free jet test configuration are discussed.

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Gokcen, Tahir, Balboni, John A., Hartman, Grover J.. 2016-06-13. CFD Simulations for Arc-Jet Panel Testing Capability Development Using Semi-Elliptical Nozzles. https://ntrs.nasa.gov/citations/20190000380

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