Abstract
Dr. L. Moon, Bell Aerospace Company, has made a series of mean velocity and stagnation pressure measurements from which local free-stream static pressure was determined for a coaxial air jet; I believe these data will interest you. We feel the results demonstrate that even for the simple coaxial injector geometry frequently used in H2/O2 rockets, conventional modeling techniques do not apply.
Work supported by NASA-Lewis Research Center, under Contract NAS3-16798, Dr. R. J. Priem, Project Manager.
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References
Moon, L. F., “Experimental Investigation of Turbulent Velocity and Static Pressure in the Developing Region of Coaxial Jets,” Eleventh JANNAF Combustion Meeting, Pasadena, California, September 1974.
Morgenthaler, J. H., Moon, L. F., and Stepien, W. R., “Developing a Gas Rocket Performance Prediction Technique,” NAS3-16798, Final Report in Preparation.
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© 1975 Plenum Press, New York
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Morgenthaler, J.H. (1975). Velocity and Pressure Characterization of Coaxial Jets. In: Murthy, S.N.B. (eds) Turbulent Mixing in Nonreactive and Reactive Flows. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-8738-5_9
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DOI: https://doi.org/10.1007/978-1-4615-8738-5_9
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