Multi Dimensional Combustion Instability Analysis Of Solid Propellant Rocket Motors PDF Download
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Author | : T. J. Chung |
Publisher | : |
Total Pages | : 47 |
Release | : 1985 |
Genre | : |
ISBN | : |
Download Multi-Dimensional Combustion Instability Analysis of Solid Propellant Rocket Motors Book in PDF, ePub and Kindle
Analytical models are developed for the multi-dimensional combustion instability analysis of solid propellant rocket motors. This research was motivated by the need for improvement of the current practice in combusiton instability analysis. For example, the burning rates and response functions are affected by the extremely complex flowfield. The flow is three-dimensional or at least two-dimensional in axisymmetric geometries; vortex motions and turbulent flows must be adequately calculated; the coupling mechanism of acoustic and hydrodynamic wave oscillations and particle damping should be clarified. These flowfield phenomena, after all, are originated from the flame zone activities - oscillatory behavior of all field variables such as temperature, velocity, pressure, density of the gas, and fuel fractions. The response functions, which serve as boundary conditions for the flowfield can be calculated from the first and second order perturbation eigenvalue analyses of the flame zone governing equations. The effect of velocity coupling appears, naturally, in the second order (nonlinear) solutions. All calculations are carried out using the finite element method. Some of the findings are summarized.
Author | : T. J. Chung |
Publisher | : |
Total Pages | : 40 |
Release | : 1982 |
Genre | : |
ISBN | : |
Download Recent Advances in Combustion Instability Analysis for Solid Propellant Rocket Motors Book in PDF, ePub and Kindle
Three-dimensional combustion stability integrals are derived with effects of viscosity and vorticity incorporated. For clarity of presentation, the particle distributions in gas dynamics are not considered at this time. It is suggested that the finite element method can be utilized to advantage for complicated geometries and boundary conditions. Some of the initial finite element calculations are demonstrated for an illustrative purpose, pending a full scale numerical applications in the future. (Author).
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 50 |
Release | : 2018-07-02 |
Genre | : |
ISBN | : 9781722159733 |
Download Development of a Computerized Analysis for Solid Propellant Combustion Instability with Turbulence Book in PDF, ePub and Kindle
A multi-dimensional numerical model has been developed for the unsteady state oscillatory combustion of solid propellants subject to acoustic pressure disturbances. Including the gas phase unsteady effects, the assumption of uniform pressure across the flame zone, which has been conventionally used, is relaxed so that a higher frequency response in the long flame of a double-base propellant can be calculated. The formulation is based on a premixed, laminar flame with a one-step overall chemical reaction and the Arrhenius law of decomposition with no condensed phase reaction. In a given geometry, the Galerkin finite element solution shows the strong resonance and damping effect at the lower frequencies, similar to the result of Denison and Baum. Extended studies deal with the higher frequency region where the pressure varies in the flame thickness. The nonlinear system behavior is investigated by carrying out the second order expansion in wave amplitude when the acoustic pressure oscillations are finite in amplitude. Offset in the burning rate shows a negative sign in the whole frequency region considered, and it verifies the experimental results of Price. Finally, the velocity coupling in the two-dimensional model is discussed. Chung, T. J. and Park, O. Y. Unspecified Center NAG8-627...
Author | : Martin Summerfield |
Publisher | : AIAA |
Total Pages | : 922 |
Release | : 1992 |
Genre | : Solid propellants |
ISBN | : 9781600863967 |
Download Nonsteady Burning and Combustion Stability of Solid Propellants Book in PDF, ePub and Kindle
Author | : Louis A. Povinelli |
Publisher | : |
Total Pages | : 36 |
Release | : 1966 |
Genre | : Solid propellant rockets |
ISBN | : |
Download One-dimensional Nonlinear Model for Determining Combustion Instability in Solid Propellant Rocket Motors Book in PDF, ePub and Kindle
Author | : David T. Harrje |
Publisher | : |
Total Pages | : 668 |
Release | : 1972 |
Genre | : Liquid propellant rockets |
ISBN | : |
Download Liquid Propellant Rocket Combustion Instability Book in PDF, ePub and Kindle
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.
Author | : Jeffrey M. Grenda |
Publisher | : |
Total Pages | : |
Release | : 1992 |
Genre | : |
ISBN | : |
Download Multi-dimensional Analysis of Combustion Instabilities in Liquid Rocket Motors Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 668 |
Release | : 1972 |
Genre | : Space vehicles |
ISBN | : |
Download Liquid Propellant Rocket Combustion Instability Book in PDF, ePub and Kindle
Author | : Vigor Young |
Publisher | : AIAA |
Total Pages | : 606 |
Release | : 1995 |
Genre | : Liquid propellant rockets |
ISBN | : 9781600864186 |
Download Liquid Rocket Engine Combustion Instability Book in PDF, ePub and Kindle
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.
Author | : Gary A. Flandro |
Publisher | : |
Total Pages | : 354 |
Release | : 1972 |
Genre | : |
ISBN | : |
Download The Influence of Mean Flow on Rocket Motor Combustion Instability. Volume I. Basic Analysis, Mean Flow Application to the T-Burner. Volume II. Effect of Turbulence on Acoustic Waves in a Cavity. Volume III. Vortex Generated Sound in Solid Propellant Book in PDF, ePub and Kindle
The report consists of two problems related to acoustic combustion instability in solid propellant rockets. In the first problem, coupled acoustic cavities with mass flux across a common boundary are studied. Since the propellant grain in a solid rocket motor may assume various configurations to meet specific performance criteria, physical models considering two or more wave-carrying systems coupled together so that acoustic motion of each is affected by the other are required in the study of acoustic instability in some motor designs. In the second problem, linear analyses employing both one-dimensional and three-dimensional flow models of the T-burner are studied to resolve which is the more appropriate representation of the growth of acoustic models yield an identical expression for the acoustic growth rate of dominant longitudinal modes in the T-burner if properly formulated. (Author).