Shock Waves Analysis of the Novel Intake Design System for a Scramjet Propulsion
| Autor: | Mohammed Fares, Sharul Sham Dol, Mohanad Tarek Mohamed, Abdulla Khamis Alhassani |
|---|---|
| Rok vydání: | 2021 |
| Předmět: |
Shock wave
Materials science 020209 energy 02 engineering and technology Mechanics Propulsion Combustion 01 natural sciences 010305 fluids & plasmas Computer Science Applications symbols.namesake Mach number Control and Systems Engineering 0103 physical sciences 0202 electrical engineering electronic engineering information engineering symbols Oblique shock Supersonic speed Scramjet Gas compressor |
| Zdroj: | WSEAS TRANSACTIONS ON SYSTEMS. 20:67-75 |
| ISSN: | 2224-2678 1109-2777 |
| Popis: | The supersonic combustion scramjet in the inlet applies the shock waves compression mechanism tosubstitute the actual compressor from a gas turbine engine. The scramjet works with combustion of fuel throughthe air stream in supersonic condition at least with Mach 5. Novel design of a scramjet intake system was madewith variations in the angle of the fins and entrance width. The best combination of diameter and inclinationangle was 1.75 m and 15 degrees, respectively. The findings were able to increase the oblique shock waveinteractions and supplicate effective combustion and reduce pressure losses for the effective application ofscramjet system, which can be significant for aerospace industry. |
| Databáze: | OpenAIRE |
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