Author:
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 26
Book Description
Analysis of Injection-velocity Effects on Rocket Motor Dynamics and Stability [with List of References]
Author:
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 26
Book Description
Analysis of Injection-velocity Effects on Rocket Motor Dynamics and Stability
Author: Herbert G. Hurrell
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 32
Book Description
Analysis of Injection-velocity Effects on Rocket Motor Dynamics and Stability
Author: Herbert G. Hurrell
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 40
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
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 : 20
Book Description
Publisher:
ISBN:
Category : Liquid oxygen
Languages : en
Pages : 20
Book Description
List of Selected References on NASA Programs
Author: Library of Congress. Science and Technology Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 244
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 244
Book Description
Theory and Analysis of the Dynamic Stability of Missiles
Author: Robert L. Swaim
Publisher:
ISBN: 9781934939437
Category : Science
Languages : en
Pages : 144
Book Description
Chapter titles are ...(1) Introduction ...(2) Analysis: Thrust Forces and Moments ...(3) Sloshing Propellant Forces and Moments ...(4) Engine Inertia Forces and Moments ...(5) Aerodynamic Forces and Moments ...(6) References ...(7) Appendix A: Structural Dynamics ...(8) Appendix B: Engine Inertia ...(9) Appendix uFuel Sloshing ...(10) Appendix D: Aerodynamic Forces ...(11) Appendix E: Determinant Elements.
Publisher:
ISBN: 9781934939437
Category : Science
Languages : en
Pages : 144
Book Description
Chapter titles are ...(1) Introduction ...(2) Analysis: Thrust Forces and Moments ...(3) Sloshing Propellant Forces and Moments ...(4) Engine Inertia Forces and Moments ...(5) Aerodynamic Forces and Moments ...(6) References ...(7) Appendix A: Structural Dynamics ...(8) Appendix B: Engine Inertia ...(9) Appendix uFuel Sloshing ...(10) Appendix D: Aerodynamic Forces ...(11) Appendix E: Determinant Elements.
Solid Rocket Motor Performance Analysis and Prediction
Author: William H. Miller
Publisher:
ISBN:
Category : Solid propellant rockets
Languages : en
Pages : 124
Book Description
Publisher:
ISBN:
Category : Solid propellant rockets
Languages : en
Pages : 124
Book Description
Research and Development Technical Handbook
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 838
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 838
Book Description
Liquid Rocket Engine Combustion Instability
Author: Vigor Yang
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 600
Book Description
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 NASAs Liquid Rocket Combustion Instability (NASA SP-194) in 1972. Improved computational and experimental techniques, coupled with a number of experiences with full-scale engines worldwide, have offered opportunities for advancement of the state of the art. 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 Chinaa first. Engineers and scientists in propulsion, power generation, and combustion instability will find the 20 chapters valuable as an extension of prior work and as a reference.
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 600
Book Description
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 NASAs Liquid Rocket Combustion Instability (NASA SP-194) in 1972. Improved computational and experimental techniques, coupled with a number of experiences with full-scale engines worldwide, have offered opportunities for advancement of the state of the art. 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 Chinaa first. Engineers and scientists in propulsion, power generation, and combustion instability will find the 20 chapters valuable as an extension of prior work and as a reference.