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CFD Simulations of the AEDC H3 Arc-Jet Flow: Mach 3.3 Nozzle, Flow Surveys, Wedge ModelsThis paper reports computational simulations and analysis of tests in a high enthalpy arc-jet facility at Arnold Engineering Development Center. These tests were conducted using wedge models placed in a free jet downstream of a 4.5-inch diameter contoured Mach 3.3 nozzle in the H3 facility. For calibration of test conditions, one wedge calibration plate instrumented with an array of pressure and coaxial thermocouple heat flux gages, one stagnation pressure probe and two null-point heat flux calorimeters were used. The pitot pressure and null-point probe measurements give experimental surveys of the test flow, providing assessment of the flow uniformity and valuable data for flow characterization. The present analysis comprises computational fluid dynamics simulations of the nonequilibrium flowfield in the facility nozzle, into the test box and over the wedge models, and comparisons with the experimental measurements. Several issues related to testing are considered: test flow characterization, prediction of surface quantities for three wedge models, effects of model shape change and test article recession, and prediction of surface quantities for the test articles with two circular cavities. These simulations take into account non-uniform total enthalpy profiles at the nozzle inlet as well as the expansion waves emanating from the nozzle exit and their effects on the wedge model flowfields.
Document ID
20240008232
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Tahir Gokcen
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Jonathan D. Morgan
(Ames Research Center Mountain View, United States)
Joseph D. Williams
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Todd R. White
(Ames Research Center Mountain View, United States)
Donald T. Ellerby
(Ames Research Center Mountain View, United States)
Date Acquired
June 27, 2024
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA AVIATION Forum
Location: Las Vegas, NV
Country: US
Start Date: July 29, 2024
End Date: August 2, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Arc-jet testing
Probe sweep data
CFD simulations
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