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LAP Lambert Academic Publishing
Hybrid Rocket Combustion
SR 229
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About this Product
Hybrid Rocket Combustion This book present an effort toward investigation of the local regression rate, average regression rate through the effect of oxidizer injection pressure. The concept of combustion processes presented in this book is based on Marxmann Hybrid rocket combustion for rubber based fuels. This book includes the coverage of: -Flat plate Combustion Model -Regression Rate Equation for a Cylindrical Grain -Hybrid motor and fuel Fabrications
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