Author: Leon M. Wenzel
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 18
Book Description
Analysis of Chugging in Liquid-bipropellant Rocket Engines Using Propellants with Different Vaporization Rates
Author: Leon M. Wenzel
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 18
Book Description
Analysis of Chugging in Liquid-bipropellant Rocket Engines Using Propellants with Different Vaporization Rates
Author: Leon M. Wenzel
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 12
Book Description
Experimental Verification of a Double Dead-time Model Describing Chugging in Liquid Bipropellant Rocket Engines
Author: John R. Szuch
Publisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 44
Book Description
Liquid Rocket Engine Combustion Instability
Author: Vigor Young
Publisher: AIAA
ISBN: 9781600864186
Category : Liquid propellant rockets
Languages : en
Pages : 606
Book Description
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.
Publisher: AIAA
ISBN: 9781600864186
Category : Liquid propellant rockets
Languages : en
Pages : 606
Book Description
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.
Liquid Propellant Rocket Combustion Instability
Author: David T. Harrje
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 678
Book Description
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.
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 678
Book Description
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.
Application of a Double-dead-time Model Describing Chugging to Liquid-propellant Rocket Engines Having Multielement Injectors
Author: John R. Szuch
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 44
Book Description
Double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors.
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 44
Book Description
Double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors.
Digital Computer Program for Analysis of Chugging Instabilities
Author: John R. Szuch
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 84
Book Description
Internal Combustion Processes of Liquid Rocket Engines
Author: Zhen-Guo Wang
Publisher: John Wiley & Sons
ISBN: 1118890051
Category : Technology & Engineering
Languages : en
Pages : 352
Book Description
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.
Publisher: John Wiley & Sons
ISBN: 1118890051
Category : Technology & Engineering
Languages : en
Pages : 352
Book Description
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.
NASA Technical Note
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 392
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 392
Book Description