Publication Date:
2019-07-27
Description:
This paper reports computational simulations and analysis in support of calibration tests in a high enthalpy arc-jet facility at NASA Ames Research Center. These tests were conducted using stagnation calorimeters and two different blunted wedge models with calibration plates at a wide range of conditions in the NASA Ames 10-megawatt TP3 (Test Position 3) facility. Data were obtained using four different conical nozzles with the same test configuration in which the models were placed in a free jet downstream of the nozzle. Experimental surveys of arc-jet test flow with pitot and null-point heat flux probes were also performed at several arc-heater conditions, providing assessment of the flow uniformity and valuable data for the flow characterization. The present analysis comprises computational fluid dynamics simulations of the nonequilibrium flowfield in the facility nozzle and test box, including the models tested, and comparisons with the experimental measurements. These computational simulations provide estimates of the arc-jet test environment parameters that are not measured but are needed to evaluate the performance of thermal protection system materials, along with further valuable insights into the arc-jet testing environment. Simulation results are used to estimate centerline total enthalpy, surface shear, boundary layer thickness, and boundary layer edge Mach number and to verify that specific test requirements from the Orion program are met.
Keywords:
Fluid Mechanics and Thermodynamics; Spacecraft Design, Testing and Performance
Type:
ARC-E-DAA-TN23980
,
AIAA Thermophysics Conference; Jun 22, 2015 - Jun 26, 2015; Dallas, TX; United States|AIAA Aviation and Aeronautics Forum (Aviation 2015); Jun 22, 2015 - Jun 26, 2015; Dallas, TX; United States
Format:
application/pdf
