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The purpose of this book is to give a good guideline for design and experiments calculations of supersonic ramjet in terms of diffuser, combustion chamber and converge diverge nozzle. In this book theoretical study has been used using simulation program (FORTRAN 90) to design ramjet engine and study the effect of some parameters on engine. Therefore it has been used four types of fuel (C8H18, CH4O, H2and C3H8) to study the effect of each type on engine performance by using three variable parameters (Mach Number (M), Altitude (H) and Number of Shock (KLM). Then Author

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Itimad D J Azzawi living at Leeds/ UK and is a PhD student at Leeds University in Mechanical Engineering, has been working as assistant lecturer at University of Diyala/ Iraq since 2008.

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