Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors
Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors

Author: David T. Harrje

Publisher:

Published: 1964

Total Pages: 205

ISBN-13:

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Topics include: Nonlinear theoretical approaches - longitudinal and transverse modes (calculations based on the nonlinear longitudinal mode with time-lag effects, a shock wave model of unstable rocket combustors with small time-lag effects, transverse nozzle admittance relation for finite-amplitude waves); Nonlinear combustion instability mechanisms (transverse mode nonlinear rocket motor studies, longitudinal nonlinear rocket studies using the square-motor, vapor displacement mechanism - basic experiment in the pseudo rocket, basic experiments in droplet resonant phenomena); Droplet and wake burning - mechanism for combustion instability; High subsonic mach number extensions to the linearized theory; Expressions for transverse waves; Concept in rocket baffle design.

Liquid Propellant Rocket Combustion Instability
Liquid Propellant Rocket Combustion Instability

Author: David T. Harrje

Publisher:

Published: 1972

Total Pages: 668

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.

Combustion Instability
Combustion Instability

Author: Samuel Z. Burstein

Publisher:

Published: 1962

Total Pages: 268

ISBN-13:

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The phenomena of combustion instability in the liquid propellant rocket system is characterized by cyclic variations of pressure in the feed system and combustion chamber, or depending on the magnitude of the frequency, within the chamber alone. Some previous work is discussed along with present work and results.