NASA NTRS · 19810019558
Study of an engine flow diverter system for a large scale ejector powered aircraft model
Abstract
Requirements were established for a conceptual design study to analyze and design an engine flow diverter system and to include accommodations for an ejector system in an existing 3/4 scale fighter model equipped with YJ-79 engines. Model constraints were identified and cost-effective limited modification was proposed to accept the ejectors, ducting and flow diverter valves. Complete system performance was calculated and a versatile computer program capable of analyzing any ejector system was developed.
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Springer, R. J., Langley, B., Plant, T., Hunter, L., Brock, O.. 1981-07-01. Study of an engine flow diverter system for a large scale ejector powered aircraft model. https://ntrs.nasa.gov/citations/19810019558
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