Results 141 to 150 of about 362 (183)
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Variable Structure Control of a Turbojet Engine

1986 American Control Conference, 1986
We study the fuel control problem of a single-spool turbojet engine. A transfer function approximation method is utilized to identify linear models about operating points. Then, a sliding mode control is developed to regulate the fuel flow so that the engine speed and temperature are within their physical constraints, based on the identified linear ...
Chin-Yu Chao   +2 more
openaire   +1 more source

Development study of a precooled turbojet engine

Acta Astronautica, 2010
Abstract A precooled turbojet engine has been developed by JAXA used for the hypersonic airplane and spaceplane. The subscale engine named “S-engine” whose thrust and weight are about 1.2 kN and 100 kg was designed, fabricated and tested. The components and the system firing tests under the sea-level-static condition were successfully conducted.In ...
Tetsuya Sato   +8 more
openaire   +1 more source

Working Model of Turbojet Engine

International Scientific Journal of Engineering and Management
The project made to show the working model of Turbojet Engine. The turbojet engine operates on the Brayton cycle and features four primary stages: air intake, compression, combustion, and exhaust. The turbo-jet engine is for high speeds. The working model shows how atmospheric air is taken in and compressed using a multi-stage axial or centrifugal ...
Yashwant A P   +4 more
openaire   +1 more source

Method and apparatus for quieting a turbojet engine

The Journal of the Acoustical Society of America, 1993
A noise suppressor for attachment to the aft end of an existing turbojet engine. The noise suppressor includes a free-running turbofan wheel which includes a turbine section mounted for reaction to the exhaust gas from the jet engine, and a concentric outer fan section extending within an air duct concentric with the turbofan wheel.
openaire   +1 more source

TURBOJET ENGINE ANALYZER DESIGN STUDY

1963
Abstract : Methods of determining the condition of jet engines through measurement of performance sensitive parameters are outlined. The measurements required, test procedures, data processing, interpretation of results, and tentative limits are proposed.
openaire   +1 more source

Energy, exergy, environmental and sustainability assessments of jet and hydrogen fueled military turbojet engine

International Journal of Hydrogen Energy, 2022
Özgur Balli, Håkan Caliskan
exaly  

SIMULATION OF FLOW SEPARATION IN TURBOJET ENGINE INLETS

Journal of Applied Mechanics and Technical Physics, 2022
M. F. Engulatova   +4 more
openaire   +1 more source

STARTERS FOR TURBOJET ENGINES

Journal of the American Society for Naval Engineers, 1951
openaire   +2 more sources

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