Title: Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine
Abstract: Component data on the J35-A-23 compressor and two-stage turbine were used to determine the problems in matching the two units for operatio n in a turbojet engine. Possible operating regions were determined an d an equilibrium operating line was also determined for the assumed c onditions of zero flight speed and a jet nozzle area approximately 5. 5 percent greater than the wide-open nozzle area.
Publication Year: 1951
Publication Date: 1951-08-06
Language: en
Type: article
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