Author: Leon M. WenzelPublisher:
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. WenzelPublisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 18
Book Description
Experimental Verification of a Double Dead-time Model Describing Chugging in Liquid Bipropellant Rocket Engines
Author: John R. SzuchPublisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 44
Book Description
Application of a Double-dead-time Model Describing Chugging to Liquid-propellant Rocket Engines Having Multielement Injectors
Author: John R. SzuchPublisher:
ISBN:
Category : Combustion
Languages : en
Pages : 44
Book Description
Double-dead-time model describing chugging to liquid propellant rocket engines having multielement injectors.
Liquid Propellant Rocket Combustion Instability
Author: David T. HarrjePublisher:
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.
Digital Computer Program for Analysis of Chugging Instabilities
Author: John R. SzuchPublisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 84
Book Description
Liquid Rocket Engine Combustion Instability
Author: Vigor YoungPublisher: 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.
NASA Technical Note
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 392
Book Description
Rocket Propulsion
Author: Stephen D. HeisterPublisher: Cambridge University Press
ISBN: 1108422276
Category : Science
Languages : en
Pages : 589
Book Description
Equips students with an up-to-date practical knowledge of rocket propulsion, numerous homework problems, and online self-study materials.
Effect of Propellant-feed-system Coupling and Hydraulic Parameters on Analysis of Chugging
Author: Don J. WoodPublisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 28
Book Description
Study of Turbojet Combustor Dynamics Using Sweep-frequency Data
Author: John R. SzuchPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description
The analysis of data obtained from sweep-frequency testing of the 585 turbojet combustor is discussed.Bode plots of the response of combustor pressure to sinusoidal disturbances in fuelspray- nozzle pressure are presented for a range of fuel flows. An analog simulation was developed and used to match the experimental data and to identify the combustion dynamics. The effects of primary or burning-zone fuel-to-air ratio on the system response were also investigated. The experimental data were fit by linear transfer function forms to be used in overall system studies.