Prediction of Maximum Combustion Efficiency and Thrust Force of DLR Scramjet Engine Using ANN Models

DLR scramjet engine is one of the well-known strut base parallel fuel injection engine, with significant thrust force due to low pressure loss but with slight decrease in combustion performance. The performance parameters such as combustion efficiency and thrust force are generally affected by desig...

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Veröffentlicht in:	SN computer science 2023-09, Vol.4 (5), p.508, Article 508
Hauptverfasser:	Debnath, Anupam, Roy, Bidesh
Format:	Artikel
Sprache:	eng
Schlagworte:	Algorithms Combustion efficiency Computer Imaging Computer Science Computer Systems Organization and Communication Networks Data Structures and Information Theory Efficiency Enabling Innovative Computational Intelligence Technologies for IOT Finite volume method Fuel injection Geometry Hydrogen Information Systems and Communication Service Low pressure Machine learning Mathematical models Original Research Parameters Pattern Recognition and Graphics Performance evaluation Pressure loss Qualitative research Simulation Software Engineering/Programming and Operating Systems Struts Supersonic aircraft Supersonic combustion ramjet engines Thrust Turbulence models Vision
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