Affiliation:
1. Boeing Airplane Co., Seattle, WA
Abstract
The objective of the research and development program reported by this paper was to decrease the specific fuel consumption of a small gas-turbine engine by means of an increase in pressure ratio alone. Development of a centrifugal compressor is presented, with a general description of equipment, methods, and special problems met during the tests. Results showed the required decrease in specific fuel consumption and pointed up the advantages of a straightforward development program.
Publisher
American Society of Mechanical Engineers
Cited by
1 articles.
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1. Der Radialkompressor;Axial- und Radialkompressoren;1961