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

Détails du livre:

ISBN-13:

978-3-639-76673-8

ISBN-10:

3639766733

EAN:

9783639766738

Langue du Livre:

English

de (auteur) :

Itimad Dawood Jumaah Azzawi
Kutaeba Jamil M. Al- Khishali

Nombre de pages:

120

Publié le:

30.06.2015

Catégorie:

Mécanique, Acoustique