Publication Date:
2019-08-13
Description:
With the increasing costs of physics experiments and simultaneous increase in availability and maturity of computational tools it is not surprising that computational fluid dynamics (CFD) is playing an increasingly important role, not only in post-test investigations, but also in the early stages of experimental planning. This paper describes a CFD-based effort executed in close collaboration between computational fluid dynamicists and experimentalists to develop a virtual experiment during the early planning stages of the Enhanced Injection and Mixing project at NASA Langley Research Center. This projects aims to investigate supersonic combustion ramjet (scramjet) fuel injection and mixing physics, improve the understanding of underlying physical processes, and develop enhancement strategies and functional relationships relevant to flight Mach numbers greater than 8. The purpose of the virtual experiment was to provide flow field data to aid in the design of the experimental apparatus and the in-stream rake probes, to verify the nonintrusive measurements based on NO-PLIF, and to perform pre-test analysis of quantities obtainable from the experiment and CFD. The approach also allowed for the joint team to develop common data processing and analysis tools, and to test research ideas. The virtual experiment consisted of a series of Reynolds-averaged simulations (RAS). These simulations included the facility nozzle, the experimental apparatus with a baseline strut injector, and the test cabin. Pure helium and helium-air mixtures were used to determine the efficacy of different inert gases to model hydrogen injection. The results of the simulations were analyzed by computing mixing efficiency, total pressure recovery, and stream thrust potential. As the experimental effort progresses, the simulation results will be compared with the experimental data to calibrate the modeling constants present in the CFD and validate simulation fidelity. CFD will also be used to investigate different injector concepts, improve understanding of the flow structure and flow physics, and develop functional relationships. Both RAS and large eddy simulations (LES) are planned for post-test analysis of the experimental data.
Keywords:
Fluid Mechanics and Thermodynamics
Type:
NF1676L-19299
,
Combustion; Dec 08, 2014 - Dec 11, 2014; Albuquerque, NM; United States|Propulsion Systems Hazards; Dec 08, 2014 - Dec 11, 2014; Albuquerque, NM; United States|Exhaust Plume and Signatures; Dec 08, 2014 - Dec 11, 2014; Albuquerque, NM; United States|Airbreathing Propulsion; Dec 08, 2014 - Dec 11, 2014; Albuquerque, NM; United States|JANNAF Joint Subcommittee Meeting; Dec 08, 2014 - Dec 11, 2014; Albuquerque, NM; United States
Format:
application/pdf
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