Liquid Propellant Rocket Combustion Instability
Liquid Propellant Rocket Combustion Instability

Author: David T. Harrje

Publisher:

Published: 1972

Total Pages: 678

ISBN-13:

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The solution of problems of combustion instability for more effective communication between the various workers in this field is considered. The extent of combustion instability problems in liquid propellant rocket engines and recommendations for their solution are discussed. The most significant developments, both theoretical and experimental, are presented, with emphasis on fundamental principles and relationships between alternative approaches.

Liquid Rocket Engine Combustion Instability
Liquid Rocket Engine Combustion Instability

Author: Vigor Young

Publisher: AIAA

Published: 1995

Total Pages: 606

ISBN-13: 9781600864186

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Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.

Internal Combustion Processes of Liquid Rocket Engines
Internal Combustion Processes of Liquid Rocket Engines

Author: Zhen-Guo Wang

Publisher: John Wiley & Sons

Published: 2016-05-17

Total Pages: 509

ISBN-13: 1118890051

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This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.