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Working Model of Turbojet Engine

Authors: Yashwant A P; Tanushree Kale; Nikita Mane; Purva Rupavate; Gaurav Bankar;

Working Model of Turbojet Engine

Abstract

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 compressor. The compressed air then enters the combustion chamber, where it mixes with fuel and undergoes ignition, producing high-energy exhaust gases. These gases rapidly expand through a turbine, extracting mechanical energy to drive the compressor and producing thrust as they accelerate through a nozzle to generate forward propulsion. This model serves as an educational tool, illustrating critical concepts such as the conversion of chemical energy into kinetic energy. Key Words: Turbojet Engine, Air Intake, Compression, Combustion, Exhaust, Centrifugal Compressor, Chemical Energy, Kinetic Energy.

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
0
Average
Average
Average
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