Method of Matching Components and Predicting Performance of a Turbine-propeller Engine

Method of Matching Components and Predicting Performance of a Turbine-propeller Engine
Author: Alois T. Sutor
Publisher:
Total Pages: 706
Release: 1951
Genre: Airplanes
ISBN:


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Analytical expressions are derived to show the geometric, thermodynamic, and aerodynamic relations among compressor, turbine, and exhaust nozzle for a gas-turbine engine. For a known compressor performance map, a matching method is described to show some of the design compromises that must be made when the components are to be combined into a turbine-propeller engine. A method of predicting engine performance for a range of operating conditions from known component maps is presented. An illustrative example of the matching method and the performance analysis is presented, showing some of the practical limitations of engine operation.


Method of Matching Components and Predicting Performance of a Turbine-propeller Engine
Language: en
Pages: 706
Authors: Alois T. Sutor
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

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Analytical expressions are derived to show the geometric, thermodynamic, and aerodynamic relations among compressor, turbine, and exhaust nozzle for a gas-turbi
Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 1080
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1952 - Publisher:

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Technical Note
Language: en
Pages: 462
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

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Index of NACA Technical Publications
Language: en
Pages: 274
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1953 - Publisher:

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A Selected Listing of NASA Scientific and Technical Reports for ...
Language: en
Pages: 750
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1949 - Publisher:

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