NASA NTRS · 19790004798
Evaluation of advanced regenerator systems
Abstract
The major considerations are discussed which will affect the selection of a ceramic regenerative heat exchanger for an improved 100 HP automotive gas turbine engine. The regenerator considered for this application is about 36cm in diameter. Regenerator comparisons are made on the basis of material, method of fabrication, cost, and performance. A regenerator inlet temperature of 1000 C is assumed for performance comparisons, and laboratory test results are discussed for material comparisons at 1100 and 1200 C. Engine test results using the Ford 707 industrial gas turbine engine are also discussed.
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Cook, J. A., Fucinari, C. A., Lingscheit, J. N., Rahnke, C. J.. 1978-08-01. Evaluation of advanced regenerator systems. https://ntrs.nasa.gov/citations/19790004798
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